<?xml version="1.0" encoding="UTF-8"?><!DOCTYPE article PUBLIC "-//NLM//DTD Journal Publishing DTD v3.0 20080202//EN" "http://dtd.nlm.nih.gov/publishing/3.0/journalpublishing3.dtd">
<article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" dtd-version="3.0" xml:lang="en" article-type="research article">
 <front>
  <journal-meta>
   <journal-id journal-id-type="publisher-id">
    ampc
   </journal-id>
   <journal-title-group>
    <journal-title>
     Advances in Materials Physics and Chemistry
    </journal-title>
   </journal-title-group>
   <issn pub-type="epub">
    2162-531X
   </issn>
   <issn publication-format="print">
    2162-5328
   </issn>
   <publisher>
    <publisher-name>
     Scientific Research Publishing
    </publisher-name>
   </publisher>
  </journal-meta>
  <article-meta>
   <article-id pub-id-type="doi">
    10.4236/ampc.2025.155005
   </article-id>
   <article-id pub-id-type="publisher-id">
    ampc-145078
   </article-id>
   <article-categories>
    <subj-group subj-group-type="heading">
     <subject>
      Articles
     </subject>
    </subj-group>
    <subj-group subj-group-type="Discipline-v2">
     <subject>
      Chemistry 
     </subject>
     <subject>
       Materials Science, Physics 
     </subject>
     <subject>
       Mathematics
     </subject>
    </subj-group>
   </article-categories>
   <title-group>
    Calculation and Analysis of the Thermodynamic Properties of Air-Aerosols Mixtures
   </title-group>
   <contrib-group>
    <contrib contrib-type="author" xlink:type="simple">
     <name name-style="western">
      <surname>
       Wepari Charles
      </surname>
      <given-names>
       Yaguibou
      </given-names>
     </name> 
     <xref ref-type="aff" rid="aff1"> 
      <sup>1</sup>
     </xref>
    </contrib>
    <contrib contrib-type="author" xlink:type="simple">
     <name name-style="western">
      <surname>
       Aly Rachid
      </surname>
      <given-names>
       Korbeogo
      </given-names>
     </name> 
     <xref ref-type="aff" rid="aff2"> 
      <sup>2</sup>
     </xref>
    </contrib>
    <contrib contrib-type="author" xlink:type="simple">
     <name name-style="western">
      <surname>
       Ibrahim
      </surname>
      <given-names>
       Pafadnam
      </given-names>
     </name> 
     <xref ref-type="aff" rid="aff3"> 
      <sup>3</sup>
     </xref>
    </contrib>
    <contrib contrib-type="author" xlink:type="simple">
     <name name-style="western">
      <surname>
       Niessan
      </surname>
      <given-names>
       Kohio
      </given-names>
     </name> 
     <xref ref-type="aff" rid="aff4"> 
      <sup>4</sup>
     </xref>
    </contrib>
    <contrib contrib-type="author" xlink:type="simple">
     <name name-style="western">
      <surname>
       Abdoul Karim
      </surname>
      <given-names>
       Kagone
      </given-names>
     </name> 
     <xref ref-type="aff" rid="aff5"> 
      <sup>5</sup>
     </xref>
    </contrib>
    <contrib contrib-type="author" xlink:type="simple">
     <name name-style="western">
      <surname>
       Zacharie
      </surname>
      <given-names>
       Koalaga
      </given-names>
     </name> 
     <xref ref-type="aff" rid="aff5"> 
      <sup>5</sup>
     </xref>
    </contrib>
   </contrib-group> 
   <aff id="aff1">
    <addr-line>
     aCentre Universitaire de Dori, Université Thomas Sankara, Ouagadougou, Burkina Faso
    </addr-line> 
   </aff> 
   <aff id="aff2">
    <addr-line>
     aEcole Polytechnique de Ouagadougou, Ouagadougou, Burkina Faso
    </addr-line> 
   </aff> 
   <aff id="aff3">
    <addr-line>
     aUFR Science et Technologie, Université Thomas Sankara, Ouagadougou, Burkina Faso
    </addr-line> 
   </aff> 
   <aff id="aff4">
    <addr-line>
     aEcole Normale Supérieure, Ouagadougou, Burkina Faso
    </addr-line> 
   </aff> 
   <aff id="aff5">
    <addr-line>
     aUFR Science et Technologie, Université Joseph Ki-Zerbo, Ouagadougou, Burkina Faso
    </addr-line> 
   </aff> 
   <pub-date pub-type="epub">
    <day>
     25
    </day> 
    <month>
     08
    </month>
    <year>
     2025
    </year>
   </pub-date> 
   <volume>
    15
   </volume> 
   <issue>
    05
   </issue>
   <fpage>
    75
   </fpage>
   <lpage>
    89
   </lpage>
   <history>
    <date date-type="received">
     <day>
      21,
     </day>
     <month>
      March
     </month>
     <year>
      2025
     </year>
    </date>
    <date date-type="published">
     <day>
      27,
     </day>
     <month>
      March
     </month>
     <year>
      2025
     </year> 
    </date> 
    <date date-type="accepted">
     <day>
      27,
     </day>
     <month>
      May
     </month>
     <year>
      2025
     </year> 
    </date>
   </history>
   <permissions>
    <copyright-statement>
     © Copyright 2014 by authors and Scientific Research Publishing Inc. 
    </copyright-statement>
    <copyright-year>
     2014
    </copyright-year>
    <license>
     <license-p>
      This work is licensed under the Creative Commons Attribution International License (CC BY). http://creativecommons.org/licenses/by/4.0/
     </license-p>
    </license>
   </permissions>
   <abstract>
    Circuit breakers and other electrical equipment are often exposed to operational challenges caused by dust contamination, particularly short-circuit failures. These issues are frequently linked to the deposition of aerosols containing compounds such as aluminium oxide (Al
    <sub>2</sub>O
    <sub>3</sub>), calcium oxide (CaO), iron oxide (Fe
    <sub>2</sub>O
    <sub>3</sub>), and silicon dioxide (SiO
    <sub>2</sub>) on critical components. While previous research has examined the influence of individual dust species—especially silica—on circuit breaker performance, these studies primarily focused on isolated effects, neglecting the combined thermodynamic impact of multiple aerosol constituents. In reality, environmental dust often comprises a mixture of species, including Al
    <sub>2</sub>O
    <sub>3</sub>, CaO, Fe
    <sub>2</sub>O
    <sub>3</sub>, and CO, which can vary significantly depending on the geographical context. This study aims to assess the influence of such aerosols on the thermodynamic properties of air plasma under atmospheric pressure and local thermodynamic equilibrium conditions, across a temperature range of 2000 K to 30,000 K. The properties, including mass enthalpy, specific heat at constant pressure, sound velocity, and mass density, are computed directly from the population densities of the relevant species. Results reveal that the presence of aerosol mixtures alters the thermodynamic behaviour of the arc plasma during circuit interruption. Notably, reductions in mass enthalpy, specific heat, and sound velocity are observed with increasing temperature, while specific heat increases at temperatures below 7000 K. Additionally, mass density is found to increase with temperature. These findings suggest that aerosol contamination during the interruption phase can degrade circuit breaker performance, potentially resulting in residual leakage currents or fire risks due to incomplete arc quenching.
   </abstract>
   <kwd-group> 
    <kwd>
     Composition
    </kwd> 
    <kwd>
      Density
    </kwd> 
    <kwd>
      Enthalpy
    </kwd> 
    <kwd>
      Plasma
    </kwd> 
    <kwd>
      Heat
    </kwd> 
    <kwd>
      Sound
    </kwd> 
    <kwd>
      Aerosol
    </kwd>
   </kwd-group>
  </article-meta>
 </front>
 <body>
  <sec id="s1">
   <title>1. Introduction</title>
   <p>
    <xref ref-type="bibr" rid="scirp.145078-"></xref>Dust is an environmental factor that can accelerate the ageing and malfunction of electrical equipment. The West African region, situated within the intertropical zone, extends from 4˚N to the southern edge of the Sahara (~20˚N) and from 18˚W to 20˚E (eastern border of Lake Chad) <xref ref-type="bibr" rid="scirp.145078-1">
     [1]
    </xref>. This region is a significant source of desert aerosols, which include dust particles, sand, pollen, volcanic ash, and sea spray. The transport of these particles across West Africa is largely influenced by regional atmospheric dynamics, particularly the Harmattan and monsoon winds <xref ref-type="bibr" rid="scirp.145078-1">
     [1]
    </xref>-<xref ref-type="bibr" rid="scirp.145078-4">
     [4]
    </xref>.</p>
   <p>
    <xref ref-type="bibr" rid="scirp.145078-"></xref>The chemical composition of aerosols in West Africa varies according to soil characteristics. Typically, they are composed of oxides of aluminium, calcium, iron, and silica (Al<sub>2</sub>O<sub>3</sub>, CaO, Fe<sub>2</sub>O<sub>3</sub>, and SiO<sub>2</sub>, respectively) <xref ref-type="bibr" rid="scirp.145078-5">
     [5]
    </xref>-<xref ref-type="bibr" rid="scirp.145078-12">
     [12]
    </xref>. Desert aerosols often mix with urban pollutants like hydrocarbons <xref ref-type="bibr" rid="scirp.145078-13">
     [13]
    </xref> <xref ref-type="bibr" rid="scirp.145078-14">
     [14]
    </xref> and accumulate on electrical equipment, particularly circuit breakers. Through vent holes, the mixture enters circuit breakers and deposits on the electrodes and within the breaking chamber <xref ref-type="bibr" rid="scirp.145078-15">
     [15]
    </xref> <xref ref-type="bibr" rid="scirp.145078-16">
     [16]
    </xref>. <xref ref-type="fig" rid="figFigures 1-2">
     Figures 1-2
    </xref> show dust episodes and accumulation on circuit breakers. Previous studies have demonstrated the impact of dust particles, such as silica, on circuit breaker performance. Silica significantly alters molar fractions, forming solid and liquid SiO<sub>2</sub> phases that condense on the gas generator surfaces. This process modifies the arc’s dynamic viscosity and speed <xref ref-type="bibr" rid="scirp.145078-15">
     [15]
    </xref> <xref ref-type="bibr" rid="scirp.145078-16">
     [16]
    </xref>. Aerosols can degrade electrical circuits and components within circuit breakers. However, prior studies have not addressed the combined effects of various species, including Fe<sub>2</sub>O<sub>3</sub>, CaO, Al<sub>2</sub>O<sub>3</sub>, and CO, which may be present in dust deposits depending on regional conditions. This study aims to investigate the effects of aerosols on the thermodynamic properties of plasma in the West African region.</p>
   <p>The remainder of this paper is organised as follows: Section 2 outlines the methods for computing thermodynamic properties; Section 3 discusses the effects of aerosols on these properties; and Section 4 presents the conclusions.</p>
   <fig id="fig1" position="float">
    <label>Figure 1</label>
    <caption>
     <title>Figure 1. Dust storm in Niger in 2020 (<xref ref-type="bibr" rid="scirp.145078-https://sciencepost.fr">
       https://sciencepost.fr
      </xref>).</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1511010-rId13.jpeg?20250825025921" />
   </fig>
   <fig id="fig2" position="float">
    <label>Figure 2</label>
    <caption>
     <title>Figure 2. Dust deposition on circuit breakers <xref ref-type="bibr" rid="scirp.145078-15">
       [15]
      </xref>.</title>
    </caption>
    <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1511010-rId15.jpeg?20250825025921" />
   </fig>
  </sec><sec id="s2">
   <title>2. Methods and Materials</title>
   <p>In West Africa, the period from February to April is characterised by large emissions of desert dust from the Saharan and local areas. However, the wet period from June to September and the period from December to January are characterised by small emissions of dust <xref ref-type="bibr" rid="scirp.145078-17">
     [17]
    </xref>. The most abundant chemical species in aerosols are silicon, calcium, iron, and aluminium oxides. The carbon oxide species are derived from biomass fires and fossil-fuel production. Further, silicon oxides account for up to 60% of the total mass. After silica, the most abundant oxides are aluminium (Al<sub>2</sub>O<sub>3</sub>) and ferric oxides (Fe<sub>2</sub>O<sub>3</sub>) <xref ref-type="bibr" rid="scirp.145078-9">
     [9]
    </xref> <xref ref-type="bibr" rid="scirp.145078-10">
     [10]
    </xref>. These proportions are directly linked to the texture of the soil itself. They’re typically derived from analyses conducted in various studies across a sub-region. It’s important to understand that these proportions are not static; they can vary significantly from one area to another due to differences in geology and topography. The composition and proportion of the chemical components of aerosols vary depending on the area. The mass proportions reflect desert sandstorms, regional soil composition, and human activity, with SiO<sub>2</sub> as the dominant species. The red colour of the dust in Ouagadougou indicates the presence of Fe<sub>2</sub>O<sub>3</sub>. Moreover, CaO has remarkable proportions, but less than Fe<sub>2</sub>O<sub>3</sub> in Ouagadougou. The presence of Al<sub>2</sub>O<sub>3</sub> is remarkable. We have not yet encountered work that establishes a clear composition of aerosols. Studies typically focus on mass fractions and specific chemical species based on the region <xref ref-type="bibr" rid="scirp.145078-1">
     [1]
    </xref> <xref ref-type="bibr" rid="scirp.145078-3">
     [3]
    </xref> <xref ref-type="bibr" rid="scirp.145078-8">
     [8]
    </xref>-<xref ref-type="bibr" rid="scirp.145078-10">
     [10]
    </xref>.</p>
   <p>A circuit breaker may need to operate in a polluted environment over a long duration. Our study found that aerosols were composed of silicon oxides, iron oxides, aluminium oxides, calcium oxides, and carbon monoxide. We assume that 1 g of aerosol contained the following mass percentages: 50% SiO<sub>2</sub>, 20% Fe<sub>2</sub>O<sub>3</sub>, 10% Al<sub>2</sub>O<sub>3</sub>, 5% CO, and 15% CaO. This work is entirely theoretical because we do not have the equipment for experiments.</p>
   <p>The mass fractions of the chemical elements of aerosol species that constitute the basic elements of the plasma were calculated using Equation (1) below:</p>
   <p>
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mtext>
        % 
      </mtext> 
      <mi>
        A 
      </mi> 
      <mo>
        = 
      </mo> 
      <mtext>
        % 
      </mtext> 
      <mi>
        a 
      </mi> 
      <mi>
        i 
      </mi> 
      <mi>
        r 
      </mi> 
      <mo>
        * 
      </mo> 
      <mtext>
        % 
      </mtext> 
      <msub> 
       <mi>
         A 
       </mi> 
       <mrow> 
        <mi>
          a 
        </mi> 
        <mi>
          i 
        </mi> 
        <mi>
          r 
        </mi> 
       </mrow> 
      </msub> 
      <mo>
        + 
      </mo> 
      <mtext>
        % 
      </mtext> 
      <mi>
        a 
      </mi> 
      <mi>
        e 
      </mi> 
      <mi>
        r 
      </mi> 
      <mi>
        o 
      </mi> 
      <mrow> 
       <mo>
         ( 
       </mo> 
       <mtable columnalign="left"> 
        <mtr> 
         <mtd> 
          <mtext>
            % 
          </mtext> 
          <msub> 
           <mi>
             A 
           </mi> 
           <mi>
             k 
           </mi> 
          </msub> 
          <msub> 
           <mi>
             C 
           </mi> 
           <mi>
             l 
           </mi> 
          </msub> 
          <mrow> 
           <mo>
             ( 
           </mo> 
           <mrow> 
            <mfrac> 
             <mrow> 
              <mi>
                k 
              </mi> 
              <msub> 
               <mi>
                 M 
               </mi> 
               <mi>
                 A 
               </mi> 
              </msub> 
             </mrow> 
             <mrow> 
              <msub> 
               <mi>
                 M 
               </mi> 
               <mrow> 
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                   A 
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                   C 
                 </mi> 
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                   l 
                 </mi> 
                </msub> 
               </mrow> 
              </msub> 
             </mrow> 
            </mfrac> 
           </mrow> 
           <mo>
             ) 
           </mo> 
          </mrow> 
          <mo>
            + 
          </mo> 
          <mtext>
            % 
          </mtext> 
          <msub> 
           <mi>
             A 
           </mi> 
           <mi>
             x 
           </mi> 
          </msub> 
          <msub> 
           <mi>
             D 
           </mi> 
           <mi>
             z 
           </mi> 
          </msub> 
          <mrow> 
           <mo>
             ( 
           </mo> 
           <mrow> 
            <mfrac> 
             <mrow> 
              <mi>
                x 
              </mi> 
              <msub> 
               <mi>
                 M 
               </mi> 
               <mi>
                 A 
               </mi> 
              </msub> 
             </mrow> 
             <mrow> 
              <msub> 
               <mi>
                 M 
               </mi> 
               <mrow> 
                <msub> 
                 <mi>
                   A 
                 </mi> 
                 <mi>
                   x 
                 </mi> 
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                <msub> 
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                 </mi> 
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                   z 
                 </mi> 
                </msub> 
               </mrow> 
              </msub> 
             </mrow> 
            </mfrac> 
           </mrow> 
           <mo>
             ) 
           </mo> 
          </mrow> 
          <mo>
            + 
          </mo> 
         </mtd> 
        </mtr> 
        <mtr> 
         <mtd> 
          <mtext>
            % 
          </mtext> 
          <msub> 
           <mi>
             A 
           </mi> 
           <mi>
             γ 
           </mi> 
          </msub> 
          <msub> 
           <mi>
             E 
           </mi> 
           <mi>
             β 
           </mi> 
          </msub> 
          <mrow> 
           <mo>
             ( 
           </mo> 
           <mrow> 
            <mfrac> 
             <mrow> 
              <mi>
                γ 
              </mi> 
              <msub> 
               <mi>
                 M 
               </mi> 
               <mi>
                 A 
               </mi> 
              </msub> 
             </mrow> 
             <mrow> 
              <msub> 
               <mi>
                 M 
               </mi> 
               <mrow> 
                <msub> 
                 <mi>
                   A 
                 </mi> 
                 <mi>
                   γ 
                 </mi> 
                </msub> 
                <msub> 
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                   E 
                 </mi> 
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                 </mi> 
                </msub> 
               </mrow> 
              </msub> 
             </mrow> 
            </mfrac> 
           </mrow> 
           <mo>
             ) 
           </mo> 
          </mrow> 
          <mo>
            + 
          </mo> 
          <mtext>
            % 
          </mtext> 
          <msub> 
           <mi>
             A 
           </mi> 
           <mi>
             ν 
           </mi> 
          </msub> 
          <msub> 
           <mi>
             F 
           </mi> 
           <mi>
             θ 
           </mi> 
          </msub> 
          <mrow> 
           <mo>
             ( 
           </mo> 
           <mrow> 
            <mfrac> 
             <mrow> 
              <mi>
                ν 
              </mi> 
              <msub> 
               <mi>
                 M 
               </mi> 
               <mi>
                 A 
               </mi> 
              </msub> 
             </mrow> 
             <mrow> 
              <msub> 
               <mi>
                 M 
               </mi> 
               <mrow> 
                <msub> 
                 <mi>
                   A 
                 </mi> 
                 <mi>
                   ν 
                 </mi> 
                </msub> 
                <msub> 
                 <mi>
                   F 
                 </mi> 
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                 </mi> 
                </msub> 
               </mrow> 
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             </mrow> 
            </mfrac> 
           </mrow> 
           <mo>
             ) 
           </mo> 
          </mrow> 
         </mtd> 
        </mtr> 
       </mtable> 
       <mo>
         ) 
       </mo> 
      </mrow> 
     </mrow> 
    </math> (1)</p>
   <p>
    <xref ref-type="bibr" rid="scirp.145078-"></xref>where A, B, C, D, E, and F represent chemical elements; A<sub>i</sub>B<sub>j</sub> represents the chemical species of air of mass percentage %air; 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         A 
       </mi> 
       <mi>
         ν 
       </mi> 
      </msub> 
      <msub> 
       <mi>
         F 
       </mi> 
       <mi>
         θ 
       </mi> 
      </msub> 
     </mrow> 
    </math>, 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         A 
       </mi> 
       <mi>
         k 
       </mi> 
      </msub> 
      <msub> 
       <mi>
         C 
       </mi> 
       <mi>
         l 
       </mi> 
      </msub> 
     </mrow> 
    </math>, 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         A 
       </mi> 
       <mi>
         x 
       </mi> 
      </msub> 
      <msub> 
       <mi>
         D 
       </mi> 
       <mi>
         z 
       </mi> 
      </msub> 
     </mrow> 
    </math>, and 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         A 
       </mi> 
       <mi>
         γ 
       </mi> 
      </msub> 
      <msub> 
       <mi>
         E 
       </mi> 
       <mi>
         β 
       </mi> 
      </msub> 
     </mrow> 
    </math> represent the species brought by aerosols of mass percentage %aero; 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         M 
       </mi> 
       <mrow> 
        <msub> 
         <mi>
           A 
         </mi> 
         <mi>
           k 
         </mi> 
        </msub> 
        <msub> 
         <mi>
           C 
         </mi> 
         <mi>
           l 
         </mi> 
        </msub> 
       </mrow> 
      </msub> 
     </mrow> 
    </math>, 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         M 
       </mi> 
       <mrow> 
        <msub> 
         <mi>
           A 
         </mi> 
         <mi>
           x 
         </mi> 
        </msub> 
        <msub> 
         <mi>
           D 
         </mi> 
         <mi>
           z 
         </mi> 
        </msub> 
       </mrow> 
      </msub> 
     </mrow> 
    </math>, 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         M 
       </mi> 
       <mrow> 
        <msub> 
         <mi>
           A 
         </mi> 
         <mi>
           γ 
         </mi> 
        </msub> 
        <msub> 
         <mi>
           E 
         </mi> 
         <mi>
           β 
         </mi> 
        </msub> 
       </mrow> 
      </msub> 
     </mrow> 
    </math>, 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         M 
       </mi> 
       <mrow> 
        <msub> 
         <mi>
           A 
         </mi> 
         <mi>
           ν 
         </mi> 
        </msub> 
        <msub> 
         <mi>
           F 
         </mi> 
         <mi>
           θ 
         </mi> 
        </msub> 
       </mrow> 
      </msub> 
     </mrow> 
    </math>, 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         M 
       </mi> 
       <mi>
         A 
       </mi> 
      </msub> 
     </mrow> 
    </math>, 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         M 
       </mi> 
       <mi>
         B 
       </mi> 
      </msub> 
     </mrow> 
    </math>, 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         M 
       </mi> 
       <mi>
         C 
       </mi> 
      </msub> 
     </mrow> 
    </math>, and 
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <msub> 
       <mi>
         M 
       </mi> 
       <mi>
         D 
       </mi> 
      </msub> 
     </mrow> 
    </math> represent the molar masses of the species considered; and i, j, k, l, x, z, 𝜃, 𝜈, β, and γ represent the numbers of atoms. From Equation (1), we obtain the mass percentages of the basic elements of our plasma, as listed in <xref ref-type="table" rid="table1">
     Table 1
    </xref>. The initial step in calculating the thermodynamic properties and transport coefficients is determining the equilibrium composition of the gas mixture using the principle of minimisation of the Gibbs free energy of the mixture <xref ref-type="bibr" rid="scirp.145078-16">
     [16]
    </xref> <xref ref-type="bibr" rid="scirp.145078-18">
     [18]
    </xref>-<xref ref-type="bibr" rid="scirp.145078-21">
     [21]
    </xref>. To this end, the specific chemical potential of all plasma particles must be determined <xref ref-type="bibr" rid="scirp.145078-20">
     [20]
    </xref>. Smoothed and tabulated thermodynamic data from Bonnie and Bendjebbar are used to calculate specific thermodynamic properties. The specific heat capacity, specific enthalpy, and specific entropy are obtained by Equation (2) <xref ref-type="bibr" rid="scirp.145078-22">
     [22]
    </xref> <xref ref-type="bibr" rid="scirp.145078-23">
     [23]
    </xref>:</p>
   <p>
    <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
      <mrow> 
       <mo>
         { 
       </mo> 
       <mtable columnalign="left"> 
        <mtr> 
         <mtd> 
          <mfrac> 
           <mrow> 
            <msubsup> 
             <mi>
               C 
             </mi> 
             <mi>
               P 
             </mi> 
             <mn>
               0 
             </mn> 
            </msubsup> 
            <mrow> 
             <mo>
               ( 
             </mo> 
             <mi>
               T 
             </mi> 
             <mo>
               ) 
             </mo> 
            </mrow> 
           </mrow> 
           <mi>
             R 
           </mi> 
          </mfrac> 
          <mo>
            = 
          </mo> 
          <msub> 
           <mi>
             a 
           </mi> 
           <mn>
             1 
           </mn> 
          </msub> 
          <msup> 
           <mi>
             T 
           </mi> 
           <mrow> 
            <mo>
              − 
            </mo> 
            <mn>
              2 
            </mn> 
           </mrow> 
          </msup> 
          <mo>
            + 
          </mo> 
          <msub> 
           <mi>
             a 
           </mi> 
           <mn>
             2 
           </mn> 
          </msub> 
          <msup> 
           <mi>
             T 
           </mi> 
           <mrow> 
            <mo>
              − 
            </mo> 
            <mn>
              1 
            </mn> 
           </mrow> 
          </msup> 
          <mo>
            + 
          </mo> 
          <msub> 
           <mi>
             a 
           </mi> 
           <mn>
             3 
           </mn> 
          </msub> 
          <mo>
            + 
          </mo> 
          <msub> 
           <mi>
             a 
           </mi> 
           <mn>
             4 
           </mn> 
          </msub> 
          <mi>
            T 
          </mi> 
          <mo>
            + 
          </mo> 
          <msub> 
           <mi>
             a 
           </mi> 
           <mn>
             5 
           </mn> 
          </msub> 
          <msup> 
           <mi>
             T 
           </mi> 
           <mn>
             2 
           </mn> 
          </msup> 
          <mo>
            + 
          </mo> 
          <msub> 
           <mi>
             a 
           </mi> 
           <mn>
             6 
           </mn> 
          </msub> 
          <msup> 
           <mi>
             T 
           </mi> 
           <mn>
             3 
           </mn> 
          </msup> 
          <mo>
            + 
          </mo> 
          <msub> 
           <mi>
             a 
           </mi> 
           <mn>
             7 
           </mn> 
          </msub> 
          <msup> 
           <mi>
             T 
           </mi> 
           <mn>
             4 
           </mn> 
          </msup> 
         </mtd> 
        </mtr> 
        <mtr> 
         <mtd> 
          <mfrac> 
           <mrow> 
            <msup> 
             <mi>
               H 
             </mi> 
             <mn>
               0 
             </mn> 
            </msup> 
            <mrow> 
             <mo>
               ( 
             </mo> 
             <mi>
               T 
             </mi> 
             <mo>
               ) 
             </mo> 
            </mrow> 
           </mrow> 
           <mrow> 
            <mi>
              R 
            </mi> 
            <mi>
              T 
            </mi> 
           </mrow> 
          </mfrac> 
          <mo>
            = 
          </mo> 
          <mo>
            − 
          </mo> 
          <msub> 
           <mi>
             a 
           </mi> 
           <mn>
             1 
           </mn> 
          </msub> 
          <msup> 
           <mi>
             T 
           </mi> 
           <mrow> 
            <mo>
              − 
            </mo> 
            <mn>
              2 
            </mn> 
           </mrow> 
          </msup> 
          <mo>
            + 
          </mo> 
          <msub> 
           <mi>
             a 
           </mi> 
           <mn>
             2 
           </mn> 
          </msub> 
          <mfrac> 
           <mrow> 
            <mi>
              ln 
            </mi> 
            <mrow> 
             <mo>
               ( 
             </mo> 
             <mi>
               T 
             </mi> 
             <mo>
               ) 
             </mo> 
            </mrow> 
           </mrow> 
           <mi>
             T 
           </mi> 
          </mfrac> 
          <mo>
            + 
          </mo> 
          <msub> 
           <mi>
             a 
           </mi> 
           <mn>
             3 
           </mn> 
          </msub> 
          <mo>
            + 
          </mo> 
          <msub> 
           <mi>
             a 
           </mi> 
           <mn>
             4 
           </mn> 
          </msub> 
          <mfrac> 
           <mi>
             T 
           </mi> 
           <mn>
             2 
           </mn> 
          </mfrac> 
          <mo>
            + 
          </mo> 
          <msub> 
           <mi>
             a 
           </mi> 
           <mn>
             5 
           </mn> 
          </msub> 
          <mfrac> 
           <mrow> 
            <msup> 
             <mi>
               T 
             </mi> 
             <mn>
               2 
             </mn> 
            </msup> 
           </mrow> 
           <mn>
             3 
           </mn> 
          </mfrac> 
          <mo>
            + 
          </mo> 
          <msub> 
           <mi>
             a 
           </mi> 
           <mn>
             6 
           </mn> 
          </msub> 
          <mfrac> 
           <mrow> 
            <msup> 
             <mi>
               T 
             </mi> 
             <mn>
               3 
             </mn> 
            </msup> 
           </mrow> 
           <mn>
             4 
           </mn> 
          </mfrac> 
          <mo>
            + 
          </mo> 
          <msub> 
           <mi>
             a 
           </mi> 
           <mn>
             7 
           </mn> 
          </msub> 
          <mfrac> 
           <mrow> 
            <msup> 
             <mi>
               T 
             </mi> 
             <mn>
               4 
             </mn> 
            </msup> 
           </mrow> 
           <mn>
             5 
           </mn> 
          </mfrac> 
          <mo>
            + 
          </mo> 
          <mfrac> 
           <mrow> 
            <msub> 
             <mi>
               b 
             </mi> 
             <mn>
               1 
             </mn> 
            </msub> 
           </mrow> 
           <mi>
             T 
           </mi> 
          </mfrac> 
         </mtd> 
        </mtr> 
        <mtr> 
         <mtd> 
          <mfrac> 
           <mrow> 
            <msup> 
             <mi>
               S 
             </mi> 
             <mn>
               0 
             </mn> 
            </msup> 
            <mrow> 
             <mo>
               ( 
             </mo> 
             <mi>
               T 
             </mi> 
             <mo>
               ) 
             </mo> 
            </mrow> 
           </mrow> 
           <mi>
             R 
           </mi> 
          </mfrac> 
          <mo>
            = 
          </mo> 
          <mo>
            − 
          </mo> 
          <msub> 
           <mi>
             a 
           </mi> 
           <mn>
             1 
           </mn> 
          </msub> 
          <mfrac> 
           <mrow> 
            <msup> 
             <mi>
               T 
             </mi> 
             <mrow> 
              <mo>
                − 
              </mo> 
              <mn>
                2 
              </mn> 
             </mrow> 
            </msup> 
           </mrow> 
           <mn>
             2 
           </mn> 
          </mfrac> 
          <mo>
            + 
          </mo> 
          <msub> 
           <mi>
             a 
           </mi> 
           <mn>
             2 
           </mn> 
          </msub> 
          <mfrac> 
           <mrow> 
            <msup> 
             <mi>
               T 
             </mi> 
             <mrow> 
              <mo>
                − 
              </mo> 
              <mn>
                1 
              </mn> 
             </mrow> 
            </msup> 
           </mrow> 
           <mn>
             2 
           </mn> 
          </mfrac> 
          <mo>
            + 
          </mo> 
          <msub> 
           <mi>
             a 
           </mi> 
           <mn>
             3 
           </mn> 
          </msub> 
          <mi>
            ln 
          </mi> 
          <mrow> 
           <mo>
             ( 
           </mo> 
           <mi>
             T 
           </mi> 
           <mo>
             ) 
           </mo> 
          </mrow> 
          <mo>
            + 
          </mo> 
          <msub> 
           <mi>
             a 
           </mi> 
           <mn>
             4 
           </mn> 
          </msub> 
          <mi>
            T 
          </mi> 
          <mo>
            + 
          </mo> 
          <msub> 
           <mi>
             a 
           </mi> 
           <mn>
             5 
           </mn> 
          </msub> 
          <mfrac> 
           <mrow> 
            <msup> 
             <mi>
               T 
             </mi> 
             <mn>
               2 
             </mn> 
            </msup> 
           </mrow> 
           <mn>
             2 
           </mn> 
          </mfrac> 
          <mo>
            + 
          </mo> 
          <msub> 
           <mi>
             a 
           </mi> 
           <mn>
             6 
           </mn> 
          </msub> 
          <mfrac> 
           <mrow> 
            <msup> 
             <mi>
               T 
             </mi> 
             <mn>
               3 
             </mn> 
            </msup> 
           </mrow> 
           <mn>
             3 
           </mn> 
          </mfrac> 
          <mo>
            + 
          </mo> 
          <msub> 
           <mi>
             a 
           </mi> 
           <mn>
             7 
           </mn> 
          </msub> 
          <mfrac> 
           <mrow> 
            <msup> 
             <mi>
               T 
             </mi> 
             <mn>
               4 
             </mn> 
            </msup> 
           </mrow> 
           <mn>
             4 
           </mn> 
          </mfrac> 
          <mo>
            + 
          </mo> 
          <msub> 
           <mi>
             b 
           </mi> 
           <mn>
             2 
           </mn> 
          </msub> 
         </mtd> 
        </mtr> 
       </mtable> 
      </mrow> 
     </mrow> 
    </math> (2)</p>
   <p>where R and T represent the constant of perfect gases and the temperature in Kelvin. The coefficients a<sub>i</sub> and b<sub>i</sub> for each particle are given by <xref ref-type="bibr" rid="scirp.145078-22">
     [22]
    </xref> <xref ref-type="bibr" rid="scirp.145078-23">
     [23]
    </xref>.</p>
   <p>For air-aerosol mixtures, 34 monatomic species have been considered (C, O, N, Si, Al, Fe, Ca, C<sup>+</sup>, O<sup>+</sup>, N<sup>+</sup>, Si<sup>+</sup>, Al<sup>+</sup>, Fe<sup>+</sup>, Ca<sup>+</sup>, C<sup>−</sup>, O<sup>−</sup>, N<sup>−</sup>, Si<sup>−</sup>, Al<sup>−</sup>, Fe<sup>−</sup>, C<sup>++</sup>, O<sup>++</sup>, N<sup>++</sup>, Si<sup>++</sup>, Al<sup>++</sup>, Fe<sup>++</sup>, Ca<sup>++</sup>, C<sup>+++</sup>, O<sup>+++</sup>, N<sup>+++</sup>, Si<sup>+++</sup>, Al<sup>+++</sup>, Fe<sup>+++</sup>, Ca<sup>+++</sup>) and electrons; 31 diatomic species (C<sub>2</sub>, O<sub>2</sub>, N<sub>2</sub>, Si<sub>2</sub>, Al<sub>2</sub>, Fe<sub>2</sub>, Ca<sub>2</sub> CO, CN, SiC, AlC, NO, SiO, AlO, SiN, FeO, AlN, CaO, C<sub>2</sub><sup>+</sup>, O<sub>2</sub><sup>+</sup>, N<sub>2</sub><sup>+</sup>, CO<sup>+</sup>, CN<sup>+</sup>, NO<sup>+</sup>, AlO<sup>+</sup>, CaO<sup>+</sup>, N<sub>2</sub><sup>−</sup>, C<sub>2</sub><sup>−</sup>, O<sub>2</sub><sup>−</sup>, CN<sup>−</sup>, and AlO<sup>−</sup>); and 40 polyatomic species (CO<sub>2</sub>, C<sub>3</sub>, CCN, CNC, CNN, C<sub>2</sub>O, O<sub>3</sub>, N<sub>3</sub>, NCO, NO<sub>2</sub>, N<sub>2</sub>O, NCN, SiC<sub>2</sub>, SiO<sub>2</sub>, Si<sub>2</sub>C, Si<sub>2</sub>N, Si<sub>3</sub>, AlC<sub>2</sub>, AlO<sub>2</sub>, Al<sub>2</sub>O, OCCN, C<sub>2</sub>N<sub>2</sub>, CNCOCN, C<sub>3</sub>O<sub>2</sub>, C<sub>4</sub>, NO<sub>3</sub>, N<sub>2</sub>O<sub>3</sub>, N<sub>2</sub>O<sub>4</sub>, N<sub>2</sub>O<sub>5</sub>, Al<sub>2</sub>C<sub>2</sub>, Al<sub>2</sub>O<sub>2</sub>, Al<sub>2</sub>O<sub>3</sub>, Fe(CO)<sub>5</sub>, N<sub>2</sub>O<sup>+</sup>, CO<sub>2</sub><sup>+</sup>, Al<sub>2</sub>O<sup>+</sup>, Al<sub>2</sub>O<sub>2</sub><sup>+</sup>, AlO<sub>2</sub><sup>−</sup>, NO<sub>3</sub><sup>−</sup>, and NO<sub>2</sub><sup>−</sup>).</p>
   <p>In this study, the temperature range for the equilibrium composition was 2000 - 30000 K, assuming only the gaseous phase. Metals and their components are in solid form at low temperatures. At temperatures lower than approximately 2000 K, the plasma component can be established in air. The experiments are conducted at atmospheric pressure (1 bar), and therefore, all results of the thermodynamic properties are presented in this range.</p>
   <sec id="s2_1">
    <title>2.1. Mass Density (kg/m<sup>3</sup>)</title>
    <p>Mass density is the quantity involved in the fluid mechanics equation. The density measures the amount of material contained in a given volume of plasma.</p>
    <p>The following formula in Equation (3) was used <xref ref-type="bibr" rid="scirp.145078-24">
      [24]
     </xref>.</p>
    <p>
     <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         ρ 
       </mi> 
       <mo>
         = 
       </mo> 
       <mfrac> 
        <mi>
          P 
        </mi> 
        <mrow> 
         <mi>
           R 
         </mi> 
         <mi>
           T 
         </mi> 
        </mrow> 
       </mfrac> 
       <mstyle displaystyle="true"> 
        <munderover> 
         <mo>
           ∑ 
         </mo> 
         <mrow> 
          <mi>
            i 
          </mi> 
          <mo>
            = 
          </mo> 
          <mn>
            1 
          </mn> 
         </mrow> 
         <mi>
           N 
         </mi> 
        </munderover> 
        <mrow> 
         <msub> 
          <mi>
            x 
          </mi> 
          <mi>
            i 
          </mi> 
         </msub> 
         <msub> 
          <mi>
            M 
          </mi> 
          <mi>
            i 
          </mi> 
         </msub> 
        </mrow> 
       </mstyle> 
      </mrow> 
     </math> (3)</p>
    <p>where 
     <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mi>
          x 
        </mi> 
        <mi>
          i 
        </mi> 
       </msub> 
      </mrow> 
     </math>, 
     <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mi>
          M 
        </mi> 
        <mi>
          i 
        </mi> 
       </msub> 
      </mrow> 
     </math>, P, R, T, and N represent the molar fraction, molar mass of species 
     <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mi>
        i 
      </mi> 
     </math>, pressure, molar gas constant, absolute temperature, and number of species in the plasma, respectively.</p>
   </sec>
   <sec id="s2_2">
    <title>2.2. Mass Enthalpy (J/kg)</title>
    <p>Mass enthalpy was calculated using the specific enthalpies of each particle and their molar fractions using 
     <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mi>
          x 
        </mi> 
        <mi>
          i 
        </mi> 
       </msub> 
      </mrow> 
     </math>presented in Equation (4) <xref ref-type="bibr" rid="scirp.145078-24">
      [24]
     </xref> as:</p>
    <p>
     <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         h 
       </mi> 
       <mo>
         = 
       </mo> 
       <mfrac> 
        <mn>
          1 
        </mn> 
        <mi>
          M 
        </mi> 
       </mfrac> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mrow> 
         <mstyle displaystyle="true"> 
          <munderover> 
           <mo>
             ∑ 
           </mo> 
           <mrow> 
            <mi>
              i 
            </mi> 
            <mo>
              = 
            </mo> 
            <mn>
              1 
            </mn> 
           </mrow> 
           <mi>
             N 
           </mi> 
          </munderover> 
          <mrow> 
           <msub> 
            <mi>
              x 
            </mi> 
            <mi>
              i 
            </mi> 
           </msub> 
           <mrow> 
            <mo>
              ( 
            </mo> 
            <mrow> 
             <msubsup> 
              <mi>
                H 
              </mi> 
              <mi>
                i 
              </mi> 
              <mn>
                0 
              </mn> 
             </msubsup> 
             <mo>
               + 
             </mo> 
             <msub> 
              <mi>
                H 
              </mi> 
              <mi>
                f 
              </mi> 
             </msub> 
            </mrow> 
            <mo>
              ) 
            </mo> 
           </mrow> 
          </mrow> 
         </mstyle> 
        </mrow> 
        <mo>
          ) 
        </mo> 
       </mrow> 
       <mo>
         − 
       </mo> 
       <mfrac> 
        <mrow> 
         <msub> 
          <mi>
            k 
          </mi> 
          <mi>
            b 
          </mi> 
         </msub> 
         <mi>
           T 
         </mi> 
        </mrow> 
        <mrow> 
         <mn>
           6 
         </mn> 
         <mi>
           π 
         </mi> 
         <msubsup> 
          <mi>
            λ 
          </mi> 
          <mi>
            D 
          </mi> 
          <mn>
            3 
          </mn> 
         </msubsup> 
        </mrow> 
       </mfrac> 
      </mrow> 
     </math> (4)</p>
    <p>where 
     <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mi>
        M 
      </mi> 
     </math> represents the average molar mass, 
     <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         M 
       </mi> 
       <mo>
         = 
       </mo> 
       <mstyle displaystyle="true"> 
        <munderover> 
         <mo>
           ∑ 
         </mo> 
         <mrow> 
          <mi>
            i 
          </mi> 
          <mo>
            = 
          </mo> 
          <mn>
            1 
          </mn> 
         </mrow> 
         <mi>
           N 
         </mi> 
        </munderover> 
        <mrow> 
         <msub> 
          <mi>
            x 
          </mi> 
          <mi>
            i 
          </mi> 
         </msub> 
         <msub> 
          <mi>
            M 
          </mi> 
          <mi>
            i 
          </mi> 
         </msub> 
        </mrow> 
       </mstyle> 
      </mrow> 
     </math> 
     <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msubsup> 
        <mi>
          H 
        </mi> 
        <mi>
          i 
        </mi> 
        <mn>
          0 
        </mn> 
       </msubsup> 
      </mrow> 
     </math> represents the molar enthalpy, and 
     <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mi>
          H 
        </mi> 
        <mi>
          f 
        </mi> 
       </msub> 
      </mrow> 
     </math> represents the heat of formation at 298.15 K (J/mol) <xref ref-type="bibr" rid="scirp.145078-23">
      [23]
     </xref>, and 
     <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mrow> 
        <mrow> 
         <msub> 
          <mi>
            k 
          </mi> 
          <mi>
            b 
          </mi> 
         </msub> 
         <mi>
           T 
         </mi> 
        </mrow> 
        <mo>
          / 
        </mo> 
        <mrow> 
         <mn>
           6 
         </mn> 
         <mi>
           π 
         </mi> 
         <msubsup> 
          <mi>
            λ 
          </mi> 
          <mi>
            D 
          </mi> 
          <mn>
            3 
          </mn> 
         </msubsup> 
        </mrow> 
       </mrow> 
      </mrow> 
     </math> represents the Debye-Huckel term.</p>
   </sec>
   <sec id="s2_3">
    <title>2.3. Specific Heat at Constant Pressure (J/kg/K)</title>
    <p>The specific heat ( 
     <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mi>
          C 
        </mi> 
        <mi>
          p 
        </mi> 
       </msub> 
      </mrow> 
     </math>) is the amount of energy to be supplied by heat exchange to raise the temperature of a medium by 1˚. This indicated the ability of the system to store heat. If the thermodynamic transformation of the system is performed at constant pressure, the specific heat can be calculated and given by Equation (5) as <xref ref-type="bibr" rid="scirp.145078-25">
      [25]
     </xref>.</p>
    <p>
     <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mi>
          C 
        </mi> 
        <mi>
          p 
        </mi> 
       </msub> 
       <mo>
         = 
       </mo> 
       <mrow> 
        <mo>
          ( 
        </mo> 
        <mrow> 
         <mfrac> 
          <mrow> 
           <mi>
             d 
           </mi> 
           <mi>
             h 
           </mi> 
          </mrow> 
          <mrow> 
           <mi>
             d 
           </mi> 
           <mi>
             T 
           </mi> 
          </mrow> 
         </mfrac> 
        </mrow> 
        <mo>
          ) 
        </mo> 
       </mrow> 
       <mo>
         = 
       </mo> 
       <mfrac> 
        <mrow> 
         <mi>
           h 
         </mi> 
         <mrow> 
          <mo>
            ( 
          </mo> 
          <mrow> 
           <mi>
             T 
           </mi> 
           <mo>
             + 
           </mo> 
           <mi>
             Δ 
           </mi> 
           <mi>
             T 
           </mi> 
          </mrow> 
          <mo>
            ) 
          </mo> 
         </mrow> 
         <mo>
           − 
         </mo> 
         <mi>
           h 
         </mi> 
         <mrow> 
          <mo>
            ( 
          </mo> 
          <mi>
            T 
          </mi> 
          <mo>
            ) 
          </mo> 
         </mrow> 
        </mrow> 
        <mrow> 
         <mi>
           Δ 
         </mi> 
         <mi>
           T 
         </mi> 
        </mrow> 
       </mfrac> 
      </mrow> 
     </math> (5)</p>
    <p>where 
     <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         Δ 
       </mi> 
       <mi>
         T 
       </mi> 
      </mrow> 
     </math> represents the variation in temperature ( 
     <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <mi>
         Δ 
       </mi> 
       <mi>
         T 
       </mi> 
       <mo>
         = 
       </mo> 
       <mn>
         100 
       </mn> 
       <mtext>
           
       </mtext> 
       <mi>
         K 
       </mi> 
      </mrow> 
     </math>), and 
     <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mi>
        T 
      </mi> 
     </math> represents the temperature.</p>
   </sec>
   <sec id="s2_4">
    <title>2.4. Velocity of Sound (m/s)</title>
    <p>
     <xref ref-type="bibr" rid="scirp.145078-"></xref>The velocity of sound was calculated using Equation (6) below <xref ref-type="bibr" rid="scirp.145078-26">
      [26]
     </xref>:</p>
    <p>
     <math display="inline" xmlns="http://www.w3.org/1998/Math/MathML"> <mrow> 
       <msub> 
        <mi>
          V 
        </mi> 
        <mi>
          S 
        </mi> 
       </msub> 
       <mo>
         = 
       </mo> 
       <msup> 
        <mrow> 
         <mrow> 
          <mo>
            ( 
          </mo> 
          <mrow> 
           <mfrac> 
            <mrow> 
             <mi>
               R 
             </mi> 
             <mi>
               T 
             </mi> 
            </mrow> 
            <mi>
              M 
            </mi> 
           </mfrac> 
          </mrow> 
          <mo>
            ) 
          </mo> 
         </mrow> 
        </mrow> 
        <mrow> 
         <mn>
           1 
         </mn> 
         <mo>
           / 
         </mo> 
         <mn>
           2 
         </mn> 
        </mrow> 
       </msup> 
      </mrow> 
     </math> (6)</p>
    <table-wrap id="table1">
     <label>
      <xref ref-type="table" rid="table1">
       Table 1
      </xref></label>
     <caption>
      <title>
       <xref ref-type="bibr" rid="scirp.145078-"></xref>Table 1. Mass percentage of the mixtures considered in this study.</title>
     </caption>
     <table class="MsoTableGrid custom-table" border="0" cellspacing="0" cellpadding="0"> 
      <tr> 
       <td class="custom-bottom-td custom-top-td acenter" width="10.54%"><p style="text-align:center">%Air</p></td> 
       <td class="custom-bottom-td custom-top-td aleft" width="12.75%"><p style="text-align:left">%aerosol</p></td> 
       <td class="custom-bottom-td custom-top-td aleft" width="10.96%"><p style="text-align:left">%C</p></td> 
       <td class="custom-bottom-td custom-top-td aleft" width="10.96%"><p style="text-align:left">%O</p></td> 
       <td class="custom-bottom-td custom-top-td aleft" width="10.96%"><p style="text-align:left">%N</p></td> 
       <td class="custom-bottom-td custom-top-td aleft" width="10.96%"><p style="text-align:left">%Si</p></td> 
       <td class="custom-bottom-td custom-top-td aleft" width="10.96%"><p style="text-align:left">%Al</p></td> 
       <td class="custom-bottom-td custom-top-td aleft" width="10.96%"><p style="text-align:left">%Fe</p></td> 
       <td class="custom-bottom-td custom-top-td aleft" width="10.96%"><p style="text-align:left">%Ca</p></td> 
      </tr> 
      <tr> 
       <td class="custom-top-td acenter" width="10.54%"><p style="text-align:center">100</p></td> 
       <td class="custom-top-td aleft" width="12.75%"><p style="text-align:left">0</p></td> 
       <td class="custom-top-td aleft" width="10.96%"><p style="text-align:left">0</p></td> 
       <td class="custom-top-td aleft" width="10.96%"><p style="text-align:left">22.2</p></td> 
       <td class="custom-top-td aleft" width="10.96%"><p style="text-align:left">77.8</p></td> 
       <td class="custom-top-td aleft" width="10.96%"><p style="text-align:left">0</p></td> 
       <td class="custom-top-td aleft" width="10.96%"><p style="text-align:left">0</p></td> 
       <td class="custom-top-td aleft" width="10.96%"><p style="text-align:left">0</p></td> 
       <td class="custom-top-td aleft" width="10.96%"><p style="text-align:left">0</p></td> 
      </tr> 
      <tr> 
       <td class="acenter" width="10.54%"><p style="text-align:center">99</p></td> 
       <td class="aleft" width="12.75%"><p style="text-align:left">1</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">0.021</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">22.423</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">77.022</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">0.234</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">0.053</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">0.140</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">0.107</p></td> 
      </tr> 
      <tr> 
       <td class="acenter" width="10.54%"><p style="text-align:center">90</p></td> 
       <td class="aleft" width="12.75%"><p style="text-align:left">10</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">0.214</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">24.428</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">70.02</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">2.337</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">0.53</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">1.399</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">1.072</p></td> 
      </tr> 
      <tr> 
       <td class="acenter" width="10.54%"><p style="text-align:center">80</p></td> 
       <td class="aleft" width="12.75%"><p style="text-align:left">20</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">0.429</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">26.657</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">62.240</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">4.674</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">1.058</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">2.798</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">2.144</p></td> 
      </tr> 
      <tr> 
       <td class="acenter" width="10.54%"><p style="text-align:center">50</p></td> 
       <td class="aleft" width="12.75%"><p style="text-align:left">50</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">1.072</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">33.341</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">38.900</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">11.686</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">2.647</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">6.994</p></td> 
       <td class="aleft" width="10.96%"><p style="text-align:left">5.360</p></td> 
      </tr> 
      <tr> 
       <td class="custom-bottom-td acenter" width="10.54%"><p style="text-align:center">20</p></td> 
       <td class="custom-bottom-td acenter" width="12.75%"><p style="text-align:center">80</p></td> 
       <td class="custom-bottom-td acenter" width="10.96%"><p style="text-align:center">1.715</p></td> 
       <td class="custom-bottom-td acenter" width="10.96%"><p style="text-align:center">40.026</p></td> 
       <td class="custom-bottom-td acenter" width="10.96%"><p style="text-align:center">15.560</p></td> 
       <td class="custom-bottom-td acenter" width="10.96%"><p style="text-align:center">18.698</p></td> 
       <td class="custom-bottom-td acenter" width="10.96%"><p style="text-align:center">4.234</p></td> 
       <td class="custom-bottom-td acenter" width="10.96%"><p style="text-align:center">11.191</p></td> 
       <td class="custom-bottom-td acenter" width="10.96%"><p style="text-align:center">8.576</p></td> 
      </tr> 
     </table>
    </table-wrap>
    <p>
     <xref ref-type="bibr" rid="scirp.145078-"></xref>Table 2. Comparative analysis of the thermodynamic properties.</p>
    <table class="MsoTableGrid custom-table" border="0" cellspacing="0" cellpadding="0"> 
     <tr> 
      <td class="custom-bottom-td custom-top-td acenter" width="10.30%"><p style="text-align:center">Temperature (K)</p></td> 
      <td class="custom-bottom-td custom-top-td aleft" width="29.90%" colspan="3"><p style="text-align:left">Mass density (kg∙m<sup>−</sup><sup>3</sup>)</p></td> 
      <td class="custom-bottom-td custom-top-td aleft" width="29.90%" colspan="3"><p style="text-align:left">Mass enthalpy (J∙kg<sup>−</sup><sup>1</sup>)</p></td> 
      <td class="custom-bottom-td custom-top-td aleft" width="29.90%" colspan="3"><p style="text-align:left">Specific heat (Jkg<sup>−</sup><sup>1</sup>∙K<sup>−</sup><sup>1</sup>)</p></td> 
     </tr> 
     <tr> 
      <td class="custom-top-td acenter" width="10.30%"><p style="text-align:center"></p></td> 
      <td class="custom-top-td aleft" width="9.96%"><p style="text-align:left">Boulos</p></td> 
      <td class="custom-top-td aleft" width="9.97%"><p style="text-align:left">Result</p></td> 
      <td class="custom-top-td aleft" width="9.97%"><p style="text-align:left">Ecart (%)</p></td> 
      <td class="custom-top-td aleft" width="9.96%"><p style="text-align:left">Boulos</p></td> 
      <td class="custom-top-td aleft" width="9.97%"><p style="text-align:left">Result</p></td> 
      <td class="custom-top-td aleft" width="9.97%"><p style="text-align:left">Ecart (%)</p></td> 
      <td class="custom-top-td aleft" width="9.96%"><p style="text-align:left">Boulos</p></td> 
      <td class="custom-top-td aleft" width="9.97%"><p style="text-align:left">Result</p></td> 
      <td class="custom-top-td aleft" width="9.97%"><p style="text-align:left">Ecart (%)</p></td> 
     </tr> 
     <tr> 
      <td class="acenter" width="10.30%"><p style="text-align:center">7000</p></td> 
      <td class="aleft" width="9.96%"><p style="text-align:left">3.15E−2</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">3.22E−2</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">2.17</p></td> 
      <td class="aleft" width="9.96%"><p style="text-align:left">2.59E−7</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">2.60E−7</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">0.38</p></td> 
      <td class="aleft" width="9.96%"><p style="text-align:left">14,026</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">14,050.5</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">0.17</p></td> 
     </tr> 
     <tr> 
      <td class="acenter" width="10.30%"><p style="text-align:center">10000</p></td> 
      <td class="aleft" width="9.96%"><p style="text-align:left">1.72E−2</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">1.68E−2</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">2.38</p></td> 
      <td class="aleft" width="9.96%"><p style="text-align:left">4.84E−7</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">4.83E−7</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">0.21</p></td> 
      <td class="aleft" width="9.96%"><p style="text-align:left">4867.2</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">4761.62</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">2.22</p></td> 
     </tr> 
     <tr> 
      <td class="acenter" width="10.30%"><p style="text-align:center">15000</p></td> 
      <td class="aleft" width="9.96%"><p style="text-align:left">7.75E−3</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">7.78E−3</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">0.39</p></td> 
      <td class="aleft" width="9.96%"><p style="text-align:left">1.16E−8</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">1.11E−8</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">4.50</p></td> 
      <td class="aleft" width="9.96%"><p style="text-align:left">21,652</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">19,290.8</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">12.24</p></td> 
     </tr> 
     <tr> 
      <td class="acenter" width="10.30%"><p style="text-align:center"></p></td> 
      <td class="aleft" width="9.96%"><p style="text-align:left">D’Angola</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">Result</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">Ecart</p></td> 
      <td class="aleft" width="9.96%"><p style="text-align:left">D’Angola</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">Result</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">Ecart</p></td> 
      <td class="aleft" width="9.96%"><p style="text-align:left">D’Angola</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">Result</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">Ecart</p></td> 
     </tr> 
     <tr> 
      <td class="acenter" width="10.30%"><p style="text-align:center">7000</p></td> 
      <td class="aleft" width="9.96%"><p style="text-align:left">3.100E−2</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">3.223E−2</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">3.72</p></td> 
      <td class="aleft" width="9.96%"><p style="text-align:left">2.63E−7</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">2.60E−7</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">1.16</p></td> 
      <td class="aleft" width="9.96%"><p style="text-align:left">14,053.9</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">14,050.5</p></td> 
      <td class="aleft" width="9.97%"><p style="text-align:left">0.02</p></td> 
     </tr> 
     <tr> 
      <td class="custom-bottom-td acenter" width="10.30%"><p style="text-align:center">10000</p></td> 
      <td class="custom-bottom-td aleft" width="9.96%"><p style="text-align:left">1.69E−2</p></td> 
      <td class="custom-bottom-td aleft" width="9.97%"><p style="text-align:left">1.68E−2</p></td> 
      <td class="custom-bottom-td aleft" width="9.97%"><p style="text-align:left">0.59</p></td> 
      <td class="custom-bottom-td aleft" width="9.96%"><p style="text-align:left">4.87E−7</p></td> 
      <td class="custom-bottom-td aleft" width="9.97%"><p style="text-align:left">4.83E−7</p></td> 
      <td class="custom-bottom-td aleft" width="9.97%"><p style="text-align:left">0.83</p></td> 
      <td class="custom-bottom-td aleft" width="9.96%"><p style="text-align:left">4749.75</p></td> 
      <td class="custom-bottom-td aleft" width="9.97%"><p style="text-align:left">4761.62</p></td> 
      <td class="custom-bottom-td aleft" width="9.97%"><p style="text-align:left">0.25</p></td> 
     </tr> 
    </table>
   </sec>
  </sec><sec id="s3">
   <title>3. Results and Discussions</title>
   <sec id="s3_1">
    <title>3.1. Comparison</title>
    <fig id="fig3" position="float">
     <label>Figure 3</label>
     <caption>
      <title>Figure 3. Comparison of mass density data of air plasma at atmospheric pressure.</title>
     </caption>
     <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1511010-rId78.jpeg?20250825025926" />
    </fig>
    <fig id="fig4" position="float">
     <label>Figure 4</label>
     <caption>
      <title>Figure 4. Comparison of mass enthalpy data of air plasma at atmospheric pressure.</title>
     </caption>
     <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1511010-rId79.jpeg?20250825025926" />
    </fig>
    <fig id="fig5" position="float">
     <label>Figure 5</label>
     <caption>
      <title>Figure 5. Comparison of specific heat data of air plasma at atmospheric pressure.</title>
     </caption>
     <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1511010-rId80.jpeg?20250825025926" />
    </fig>
    <p>The thermodynamic of air-aerosol mixtures under the local thermodynamic equilibrium (L.T.E) assumption were evaluated across a temperature range of 2000 K - 30000 K at atmospheric pressure. These properties depend on the plasma composition, which is determined by minimising the Gibbs free energy. The local thermodynamic equilibrium is achieved when the rate of collisional processes is much higher than the rate of radiative processes (mainly radiative recombination and spontaneous emission).</p>
    <p>
     <xref ref-type="bibr" rid="scirp.145078-"></xref>No existing data were available for the exact mixture type studied here. However, previous research has examined various plasma models, including air, nitrogen, carbon dioxide (CO<sub>2</sub>), CF<sub>3</sub>I, argon-copper, argon-aluminium, C<sub>4</sub>F<sub>7</sub>N-CO<sub>2</sub>-O<sub>2</sub>, air-PA<sub>66</sub>-copper, and C<sub>4</sub>F<sub>7</sub>N plasmas <xref ref-type="bibr" rid="scirp.145078-27">
      [27]
     </xref>-<xref ref-type="bibr" rid="scirp.145078-38">
      [38]
     </xref>. The MATLAB calculation method was validated by comparing its results with those from previous plasma studies. Thus, the properties of dry air plasma were compared with results from prior work to verify the data and equations used in these calculations <xref ref-type="bibr" rid="scirp.145078-27">
      [27]
     </xref>-<xref ref-type="bibr" rid="scirp.145078-30">
      [30]
     </xref>. The thermodynamic properties are presented in <xref ref-type="table" rid="table2">
      Table 2
     </xref>, where the mass density, mass enthalpy, and specific heat show satisfactory agreement with existing data, with an overall deviation of less than 7%. However, heat capacity showed a maximum deviation of 12.24% at 15,000 K compared to the data from Boulos et al. <xref ref-type="bibr" rid="scirp.145078-27">
      [27]
     </xref>. <xref ref-type="fig" rid="figFigures 3-5">
      Figures 3-5
     </xref> show comparisons of the results for mass density, mass enthalpy, and heat capacity with the data from Boulos et al. <xref ref-type="bibr" rid="scirp.145078-27">
      [27]
     </xref> and D’Angola et al. <xref ref-type="bibr" rid="scirp.145078-28">
      [28]
     </xref>. The discrepancies observed can be attributed to the specific data used in this calculation program. Specific enthalpies, entropies, and chemical potentials were also calculated.</p>
   </sec>
   <sec id="s3_2">
    <title>
     <xref ref-type="bibr" rid="scirp.145078-"></xref>3.2. Effect of Aerosol Concentration on Thermodynamic Properties</title>
    <p>Determining the chemical composition of plasma is essential for calculating thermodynamic properties. Previous studies have analysed the thermodynamic properties of various gas mixtures, including air <xref ref-type="bibr" rid="scirp.145078-31">
      [31]
     </xref> <xref ref-type="bibr" rid="scirp.145078-32">
      [32]
     </xref>, CO<sub>2</sub> <xref ref-type="bibr" rid="scirp.145078-33">
      [33]
     </xref>, SF<sub>6</sub> <xref ref-type="bibr" rid="scirp.145078-34">
      [34]
     </xref>, and N<sub>2</sub> <xref ref-type="bibr" rid="scirp.145078-35">
      [35]
     </xref>, and CF3I <xref ref-type="bibr" rid="scirp.145078-33">
      [33]
     </xref>.</p>
    <p>
     <xref ref-type="fig" rid="fig6">
      Figure 6
     </xref> shows the mass densities of the air plasmas contaminated by aerosols. The evolution is identical for the different plasmas. The mass density decreases with increasing temperature; this decrease is greater at low temperatures (&lt;8000 K). This is reflected by the decrease in the total density of species (rarefaction of the environment) imposed by the ideal gas law and by the presence of less massive species (atoms, ions and especially electrons) at high temperatures. These are direct consequences of the dissociation and ionisation of molecular and atomic species, which lead to the gradual disappearance of molecules and atoms with an increase in temperature <xref ref-type="bibr" rid="scirp.145078-39">
      [39]
     </xref>. The mass density of pure air coincided with the mass density of plasma containing 1% aerosols. Beyond 1%, the values of contaminated air plasmas are higher than those of pure air plasma; the more the plasma is contaminated, the higher is the increase in its mass density because they contain heavier particles than air. <xref ref-type="table" rid="table3">
      Table 3
     </xref> lists the molar masses of the neutral species in the plasma.</p>
    <table-wrap id="table2">
     <label>
      <xref ref-type="table" rid="table2">
       Table 2
      </xref></label>
     <caption>
      <title>
       <xref ref-type="bibr" rid="scirp.145078-"></xref>Table 3. Molecular weight of neutral species <xref ref-type="bibr" rid="scirp.145078-23">
        [23]
       </xref>.</title>
     </caption>
     <table class="MsoTableGrid custom-table" border="0" cellspacing="0" cellpadding="0"> 
      <tr> 
       <td class="custom-bottom-td custom-top-td acenter" width="10.27%"><p style="text-align:center">Species</p></td> 
       <td class="custom-bottom-td custom-top-td aleft" width="14.73%"><p style="text-align:left">Molecular</p></td> 
       <td class="custom-bottom-td custom-top-td aleft" width="10.25%"><p style="text-align:left">Species</p></td> 
       <td class="custom-bottom-td custom-top-td aleft" width="16.23%"><p style="text-align:left">Molecular</p></td> 
       <td class="custom-bottom-td custom-top-td aleft" width="10.25%"><p style="text-align:left">Species</p></td> 
       <td class="custom-bottom-td custom-top-td aleft" width="12.50%"><p style="text-align:left">Molecular</p></td> 
       <td class="custom-bottom-td custom-top-td aleft" width="10.25%"><p style="text-align:left">Species</p></td> 
       <td class="custom-bottom-td custom-top-td aleft" width="12.51%"><p style="text-align:left">Molecular</p></td> 
      </tr> 
      <tr> 
       <td class="custom-top-td acenter" width="10.27%"><p style="text-align:center"></p></td> 
       <td class="custom-top-td aleft" width="14.73%"><p style="text-align:left">weight (g/mol)</p></td> 
       <td class="custom-top-td aleft" width="10.25%"><p style="text-align:left"></p></td> 
       <td class="custom-top-td aleft" width="16.23%"><p style="text-align:left">weight (g/mol)</p></td> 
       <td class="custom-top-td aleft" width="10.25%"><p style="text-align:left"></p></td> 
       <td class="custom-top-td aleft" width="12.50%"><p style="text-align:left">weight (g/mol)</p></td> 
       <td class="custom-top-td aleft" width="10.25%"><p style="text-align:left"></p></td> 
       <td class="custom-top-td aleft" width="12.51%"><p style="text-align:left">weight (g/mol)</p></td> 
      </tr> 
      <tr> 
       <td class="acenter" width="10.27%"><p style="text-align:center">C</p></td> 
       <td class="aleft" width="14.73%"><p style="text-align:left">12.01070</p></td> 
       <td class="aleft" width="10.25%"><p style="text-align:left">CO</p></td> 
       <td class="aleft" width="16.23%"><p style="text-align:left">28.01010</p></td> 
       <td class="aleft" width="10.25%"><p style="text-align:left">O<sub>2</sub></p></td> 
       <td class="aleft" width="12.50%"><p style="text-align:left">31.99880</p></td> 
       <td class="aleft" width="10.25%"><p style="text-align:left">SiN</p></td> 
       <td class="aleft" width="12.51%"><p style="text-align:left">42.09220</p></td> 
      </tr> 
      <tr> 
       <td class="acenter" width="10.27%"><p style="text-align:center">N</p></td> 
       <td class="aleft" width="14.73%"><p style="text-align:left">14.00670</p></td> 
       <td class="aleft" width="10.25%"><p style="text-align:left">CN</p></td> 
       <td class="aleft" width="16.23%"><p style="text-align:left">26.01740</p></td> 
       <td class="aleft" width="10.25%"><p style="text-align:left">N<sub>2</sub></p></td> 
       <td class="aleft" width="12.50%"><p style="text-align:left">28.01340</p></td> 
       <td class="aleft" width="10.25%"><p style="text-align:left">FeO</p></td> 
       <td class="aleft" width="12.51%"><p style="text-align:left">71.84440</p></td> 
      </tr> 
      <tr> 
       <td class="acenter" width="10.27%"><p style="text-align:center">O</p></td> 
       <td class="aleft" width="14.73%"><p style="text-align:left">15.99940</p></td> 
       <td class="aleft" width="10.25%"><p style="text-align:left">SiC</p></td> 
       <td class="aleft" width="16.23%"><p style="text-align:left">40.09620</p></td> 
       <td class="aleft" width="10.25%"><p style="text-align:left">Si<sub>2</sub></p></td> 
       <td class="aleft" width="12.50%"><p style="text-align:left">56.17100</p></td> 
       <td class="aleft" width="10.25%"><p style="text-align:left">AlN</p></td> 
       <td class="aleft" width="12.51%"><p style="text-align:left">40.98828</p></td> 
      </tr> 
      <tr> 
       <td class="acenter" width="10.27%"><p style="text-align:center">Si</p></td> 
       <td class="aleft" width="14.73%"><p style="text-align:left">28.08550</p></td> 
       <td class="aleft" width="10.25%"><p style="text-align:left">AlC</p></td> 
       <td class="aleft" width="16.23%"><p style="text-align:left">38.99224</p></td> 
       <td class="aleft" width="10.25%"><p style="text-align:left">Al<sub>2</sub></p></td> 
       <td class="aleft" width="12.50%"><p style="text-align:left">53.96308</p></td> 
       <td class="aleft" width="10.25%"><p style="text-align:left">CO<sub>2</sub></p></td> 
       <td class="aleft" width="12.51%"><p style="text-align:left">44.00950</p></td> 
      </tr> 
      <tr> 
       <td class="acenter" width="10.27%"><p style="text-align:center">Al</p></td> 
       <td class="aleft" width="14.73%"><p style="text-align:left">26.98154</p></td> 
       <td class="aleft" width="10.25%"><p style="text-align:left">NO</p></td> 
       <td class="aleft" width="16.23%"><p style="text-align:left">30.00610</p></td> 
       <td class="aleft" width="10.25%"><p style="text-align:left">Fe<sub>2</sub></p></td> 
       <td class="aleft" width="12.50%"><p style="text-align:left">111.6900</p></td> 
       <td class="aleft" width="10.25%"><p style="text-align:left">C<sub>3</sub></p></td> 
       <td class="aleft" width="12.51%"><p style="text-align:left">36.03210</p></td> 
      </tr> 
      <tr> 
       <td class="custom-bottom-td acenter" width="10.27%"><p style="text-align:center">Fe</p></td> 
       <td class="custom-bottom-td aleft" width="14.73%"><p style="text-align:left">55.84500</p></td> 
       <td class="custom-bottom-td aleft" width="10.25%"><p style="text-align:left">SiO</p></td> 
       <td class="custom-bottom-td aleft" width="16.23%"><p style="text-align:left">44.08490</p></td> 
       <td class="custom-bottom-td aleft" width="10.25%"><p style="text-align:left">C<sub>2</sub></p></td> 
       <td class="custom-bottom-td aleft" width="12.50%"><p style="text-align:left">24.02140</p></td> 
       <td class="custom-bottom-td aleft" width="10.25%"><p style="text-align:left">AlO</p></td> 
       <td class="custom-bottom-td aleft" width="12.51%"><p style="text-align:left">42.98094</p></td> 
      </tr> 
     </table>
    </table-wrap>
    <fig id="fig6" position="float">
     <label>Figure 6</label>
     <caption>
      <title>Figure 6. Evolution of the mass density of the plasma according to the percentage of aerosols, units: kg/m<sup>3</sup>.</title>
     </caption>
     <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1511010-rId81.jpeg?20250825025927" />
    </fig>
    <p>The enthalpy curves (<xref ref-type="fig" rid="fig7">
      Figure 7
     </xref>) show rapid phases of evolution that correspond to the reactivity of the medium and to the dissociation and ionisation phenomena. Enthalpy varies inversely with mass density, and therefore, the enthalpy of the air plasma is greater than that of the polluted air plasma. In other words, the more polluted the air, the greater is the decrease in enthalpy.</p>
    <fig id="fig7" position="float">
     <label>Figure 7</label>
     <caption>
      <title>
       <xref ref-type="bibr" rid="scirp.145078-"></xref>Figure 7. Evolution of the mass enthalpy of the plasma according to the percentage of aerosols, units: J/kg.</title>
     </caption>
     <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1511010-rId82.jpeg?20250825025927" />
    </fig>
    <p>
     <xref ref-type="fig" rid="fig8">
      Figure 8
     </xref> shows that specific heat strongly depends on the nature of the mixture and temperature, with the appearance of peaks in the regions where the enthalpy varies rapidly. The curves show the same pattern with the first peak at ~3500 K and the second at ~7000 K for up to 50% aerosols. Beyond this proportion, the peak gradually shifted towards lower temperatures (e.g. the peak was ~5500 K between 80% and 100% aerosols). The third peak occurs at ~15,000 K, where the peak moved slightly with an increase in the aerosol rate. These peaks represent the dissociation (of molecules) and ionisation (of atoms). The first peak (at ~3500 K) corresponds to the dissociation of CO<sub>2</sub>, FeO, AlC, CN, SiC, AlC, SiN, NO, O<sub>2</sub>, Al<sub>2</sub>O, and SiO<sub>3 </sub>molecules. For example, O<sub>2</sub>, CO<sub>2</sub>, and Al<sub>2</sub>O dissociate at ~3500, 3400, and 4000 K <xref ref-type="bibr" rid="scirp.145078-40">
      [40]
     </xref>. Al<sub>2</sub> and Fe<sub>2</sub> dissociate below 3000 K <xref ref-type="bibr" rid="scirp.145078-40">
      [40]
     </xref>, and C<sub>3</sub> and C<sub>2</sub> dissociate at ~5000 K <xref ref-type="bibr" rid="scirp.145078-40">
      [40]
     </xref>. The peak at ~5500 K for aerosols with mass percentages between 80% and 100% can be attributed to the dissociation of AlO and SiO. The dissociation peak of SiO appeared at ~5700 K at 1 atm <xref ref-type="bibr" rid="scirp.145078-41">
      [41]
     </xref>.</p>
    <p>The second peak corresponds to the dissociation of the CO and N<sub>2</sub> molecules. CO and N<sub>2</sub> dissociate at ~7000 K <xref ref-type="bibr" rid="scirp.145078-40">
      [40]
     </xref>. The first ionisation of the Al atom occurs at 9000 K <xref ref-type="bibr" rid="scirp.145078-42">
      [42]
     </xref> <xref ref-type="bibr" rid="scirp.145078-43">
      [43]
     </xref>, whereas that of the Fe atom occurs between 8500 K and 9000 K <xref ref-type="bibr" rid="scirp.145078-44">
      [44]
     </xref>. Si and Ca ionise at the same temperature. The Al, Fe, Si, and Ca atoms ionise rapidly before the C, O, and N atoms because of their low ionisation energies (Ei0<sub>Al</sub> = 5.986 eV, Ei0<sub>Ca</sub> = 6.113 eV, Ei0<sub>Fe</sub> = 7.902 eV, Ei0<sub>Si</sub> = 8.151 eV, Ei0<sub>C</sub> = 11.26 eV, Ei0<sub>O</sub> = 13.628 eV, and Ei0<sub>N</sub> = 14.55 eV). The third peak corresponds to the ionisation of C, O, and N atoms. The first ionisation of O and N is ~15,000 K <xref ref-type="bibr" rid="scirp.145078-44">
      [44]
     </xref>.</p>
    <p>The second ionisation of Al and Fe occurs around 19,000 K <xref ref-type="bibr" rid="scirp.145078-42">
      [42]
     </xref> <xref ref-type="bibr" rid="scirp.145078-44">
      [44]
     </xref>. The temperature corresponding to the second ionisation of C, O, and N was ~30,000 K <xref ref-type="bibr" rid="scirp.145078-40">
      [40]
     </xref> <xref ref-type="bibr" rid="scirp.145078-44">
      [44]
     </xref>. The first and second ionisations of Si and Ca were observed in the same temperature zones as iron and aluminium because of their similar ionisation energies. The effect of the aerosols was clear over the entire temperature range. Modifications to the locations of the main dissociation peaks are clearly observed. The movement of the peaks at low temperatures can be attributed to the chemistry. For example, for a 20% air-80% aerosol mixture, a peak was detected at ~5500 K, which can be attributed to the dissociation of AlO and SiO. Therefore, aerosols cause a decrease in specific heat because of the small energy ionisation of metals, except at temperatures below 7000 K. A high heat capacity means that the plasma can absorb more thermal energy for a given increase in temperature. This is beneficial for arc cooling, as a large portion of the arc’s energy can be “stored” in the processes of dissociation and ionization rather than directly resulting in a temperature increase that would maintain the conductive plasma. These results show that the presence of aerosols leads to a slight increase in heat capacity. So a slight cooling of the plasma. The carbon released by the decomposition of CO can deposit as soot on insulating surfaces or contacts. These soot deposits can create undesirable conduction paths, leading to flashovers or a reduction in the dielectric strength of the insulators. In the presence of metallic vapors from the contacts, metallic carbides can form, also affecting the surfaces.</p>
    <p>The presence of CO and its decomposition products can reduce the insulating capacity of the gaseous medium. Carbon particles can act as sites of electric field concentration, facilitating new discharges.</p>
    <fig id="fig8" position="float">
     <label>Figure 8</label>
     <caption>
      <title>Figure 8. Evolution of the specific heat of the plasma according to the percentage of aerosols, units: J/kg/K.</title>
     </caption>
     <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1511010-rId83.jpeg?20250825025927" />
    </fig>
    <p>
     <xref ref-type="fig" rid="fig9">
      Figure 9
     </xref> shows the evolution of the sound velocity spread in air-aerosol plasmas, which decreases with the percentage of aerosols in the mixture. This decrease in sound propagation can be explained by heavy particles present in the polluted plasma. The higher the rate of contamination, the heavier is the plasma. This decreases the velocity.</p>
    <fig id="fig9" position="float">
     <label>Figure 9</label>
     <caption>
      <title>Figure 9. Evolution of the sound velocity of the plasma according to the percentage of aerosols, units: m/s.</title>
     </caption>
     <graphic mimetype="image" position="float" xlink:type="simple" xlink:href="https://html.scirp.org/file/1511010-rId84.jpeg?20250825025927" />
    </fig>
   </sec>
  </sec><sec id="s4">
   <title>4. Conclusions</title>
   <p>
    <xref ref-type="bibr" rid="scirp.145078-"></xref>This study examined the effect of aerosols on the thermodynamic properties of air plasma in a state of local thermodynamic equilibrium. Findings indicate that plasma density increases, whereas enthalpy, specific heat, and sound velocity all decrease, as the aerosol concentration in the mixture rises. Specific heat increased at temperatures below 7000 K and decreased at higher temperatures, with notable peaks at approximately 3500 K, 7000 K, and 15,000 K. Mass specific enthalpy is a key indicator of the arc plasma’s energy state. Rapid reduction of this value is the fundamental goal of all arc extinction mechanisms in a circuit breaker to ensure reliable and safe current interruption. However, the presence of metal oxides can reduce the mass enthalpy and heat capacity at a given temperature. A potentially lower specific enthalpy and heat capacity would make arc quenching more difficult. The plasma remains conductive for longer, which extends the duration of the electric arc. A longer arc duration and sustained high temperatures increase the erosion of the circuit breaker’s contacts, reducing their lifespan and potentially their reliability. In extreme cases, excessive oxide accumulation and unfavorable changes in plasma properties can lead to a failure to interrupt the circuit, with serious consequences for the electrical grid and equipment.</p>
   <p>This theoretical analysis demonstrates that aerosols significantly impact plasma characteristics, including density, mass enthalpy, heat capacity, and sound velocity. Moreover, the plasma must be a good electrical insulator at low temperatures to facilitate the transient recovery voltage and to avoid restrikes.</p>
   <p>While thermodynamic properties alone are insufficient to determine a circuit breaker’s interruption capacity, they provide insight into the impact of aerosols on such capacity. Future studies should investigate the transport proprieties the dielectric strength properties, density variations, energy fluxes, and radiation effects, conducting experiments to comprehensively characterise plasma properties, including the influence of solid-phase aerosols.</p>
  </sec>
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