<?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><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/ampc.2023.135007</article-id><article-id pub-id-type="publisher-id">AMPC-125335</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Chemistry&amp;Materials Science</subject><subject> Physics&amp;Mathematics</subject></subj-group></article-categories><title-group><article-title>
 
 
  Study of the Thermodynamic Properties of Thermal Plasmas of Fluoroalkylamine-Air Mixtures
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Pafadnam</surname><given-names>Ibrahim</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Kohio</surname><given-names>Nièssan</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>Yaguibou</surname><given-names>Wêpari Charles</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>Kagoné</surname><given-names>Abdoul Karim</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>Koalaga</surname><given-names>Zacharie</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>André</surname><given-names>Pascal</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref></contrib></contrib-group><aff id="aff2"><addr-line>Université Clermont Auvergne, CNRS, Laboratoire de Physique de Clermont, Clermont-Ferrand, France</addr-line></aff><aff id="aff1"><addr-line>Université Joseph Ki-Zerbo, Laboratoire de Matériaux Environnement, Ouagadougou, Burkina Faso</addr-line></aff><pub-date pub-type="epub"><day>15</day><month>05</month><year>2023</year></pub-date><volume>13</volume><issue>05</issue><fpage>85</fpage><lpage>100</lpage><history><date date-type="received"><day>25,</day>	<month>January</month>	<year>2023</year></date><date date-type="rev-recd"><day>28,</day>	<month>May</month>	<year>2023</year>	</date><date date-type="accepted"><day>31,</day>	<month>May</month>	<year>2023</year></date></history><permissions><copyright-statement>&#169; 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><p>
 
 
  Knowledge of thermodynamic properties as well as parameters such as energy density and power flow 
  is
  important for modeling thermal plasmas of fluoroalkylamine-air mixtures. In this paper, these thermodynamic properties of fluoroalkylamine-air mixture plasmas are calculated in a temperature range of 500 K to 20
  ,
  000 K at atmospheric pressure and local thermodynamic equilibrium (LTE). The Gibbs free energy minimization method is used to determine the chemical equilibrium compositions of the plasmas that are needed to calculate the thermodynamic properties. These thermodynamic properties are then used to calculate the energy density and power flow of these plasmas. The variation of the energy density is related to the variations of the density and mass enthalpy. We notice that, this energy density increases with the percentage of air in the mixture for temperatures higher than 7000 K. The power flow, which depend
  s
   also on density, enthalpy mass and sound speed, increases with the percentage of air in the same temperature range. Energy density and power flow results show that increasing air percentage in the mixture can be 
  more interesting for damaging gaseous chemical species such as CF<sub>2</sub>, CO, HCN, and HF appearing at low temperatures with high concentrations.
 
</p></abstract><kwd-group><kwd>Fluoroalkylamine</kwd><kwd> Thermodynamic Properties</kwd><kwd> Chemical Composition</kwd><kwd> En-ergy Density</kwd><kwd> Power Flow</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>The environmental and climatic issues related to toxic waste management are not only ecological but also health issue. The use of thermal plasmas, through specific plasma torches for toxic waste destruction, is so promising [<xref ref-type="bibr" rid="scirp.125335-ref1">1</xref>] . Numerous theoretical and experimental studies have been carried out to understand very well these reactive media [<xref ref-type="bibr" rid="scirp.125335-ref2">2</xref>] - [<xref ref-type="bibr" rid="scirp.125335-ref8">8</xref>] . Indeed, active principles containing fluorinated organic components such as fluoroalkylamines or pyrimidine-based molecules are promising in the agricultural field (pesticides and herbicides) and pharmacology (antibiotics) [<xref ref-type="bibr" rid="scirp.125335-ref9">9</xref>] . The massive use of these molecules will result in a massive increase in waste containing these types of molecules. Developed countries have restrictive waste management policies, which is not the case in developing countries. In these countries, we are assisting in a proliferation of waste open air area storage from some others countries [<xref ref-type="bibr" rid="scirp.125335-ref10">10</xref>] . These practices have a lot of consequences on the environment like air, soil and water pollution. This could affect also human health. One of the solutions which could give better satisfaction about solid waste is use of plasma torches. These torches could reach high temperatures (5000 K to 20,000 K). However, the use of these means of treatment is not without danger because some toxic or lethal molecules could result from it. In order to understand these difficulties, we propose to study the air influence on thermodynamic properties as well as parameters such as energy density and power flow of a plasma based on fluoroalkylamines (trifluoroethylamine: C<sub>2</sub>H<sub>4</sub>F<sub>3</sub>N, Nonafluoropentylamine: C<sub>5</sub>H<sub>4</sub>F<sub>9</sub>N, ...), at atmospheric pressure and at local thermodynamic equilibrium (LTE), in a range of temperatures going from 500 K to 20,000 K. More precisely it’s calculation of density, enthalpy mass, heat mass at constant pressure and sound speed in the plasma. These parameters are necessary to determine the power flow and the energy density of the plasma. The data obtained can be used for modeling the plasma in the fluoroalkylamine-air mixture. In the framework of our study, we decided to consider only the gaseous phase, to work at atmospheric pressure, to consider that the air is made up of 20% of dioxygen and 80% of nitrogen, and that the various percentages selected are volumetric percentages. As fluoroalkylamines, we will use in this work trifluoroethylamine (C<sub>2</sub>H<sub>4</sub>F<sub>3</sub>N) and nonafluoropentylamine (C<sub>5</sub>H<sub>4</sub>F<sub>9</sub>N).</p><p>Firstly, we will describe the computational methods to get the thermodynamic properties as well as the parameters such as energy density and power flow at atmospheric pressure. Secondly, we will present the results and finally, we will conclude.</p></sec><sec id="s2"><title>2. Thermodynamic Properties Calculation Method</title><p>Thermodynamic properties as well as energy density and power flow can be deduced from the knowledge of species densities and partition functions, formulations of which are available in the literature [<xref ref-type="bibr" rid="scirp.125335-ref11">11</xref>] - [<xref ref-type="bibr" rid="scirp.125335-ref16">16</xref>] .</p><sec id="s2_1"><title>2.1. Chemical Composition of Plasmas</title><p>The plasmas studied in this work, are recorded in <xref ref-type="table" rid="table1">Table 1</xref>. The determination of the chemical composition of the plasmas is based on the Gibbs free energy minimization method using the Newton-Raphson method in the temperature range from 500 K to 20,000 K, at atmospheric pressure and at local thermodynamic equilibrium (LTE). We have considered that air is constituted with 80% of nitrogen (N<sub>2</sub>) and 20% of oxygen (O<sub>2</sub>), the other components (Ar, CO<sub>2</sub>, CH<sub>4</sub>, ...) have been totally neglected. The chemical species considered in the fluoroalkylamine-air mixture plasma are:</p><p>&#183; electrons: e<sup>−</sup>;</p><p>&#183; monoatomic species (18): C, C<sup>+</sup>, C<sup>2+</sup>, C<sup>−</sup>, F, F<sup>+</sup>, F<sup>−</sup>, H, H<sup>+</sup>, H<sup>−</sup>, N, N<sup>+</sup>, N<sup>2+</sup>, N<sup>−</sup>, O, O<sup>+</sup>, O<sup>2+</sup>, O<sup>−</sup>;</p><p>&#183; diatomic species (27): C<sub>2</sub>, F<sub>2</sub>, H<sub>2</sub>, N<sub>2</sub>, O<sub>2</sub>, CF, CH, CN, NF, NH, CO, NO, OH, HF, C 2 + , H 2 + , N 2 + , O 2 + , NO<sup>+</sup>, CF<sup>+</sup>, CH<sup>+</sup>, CN<sup>+</sup>, NH<sup>+</sup>, CO<sup>+</sup>, C 2 − , H 2 − , CN<sup>−</sup>;</p><p>&#183; polyatomic species (13): CO<sub>2</sub>, NO<sub>2</sub>, NO<sub>3</sub>, CF<sub>2</sub>, CF<sub>3</sub>, CH<sub>4</sub>, C<sub>2</sub>F, C<sub>2</sub>F<sub>2</sub>, C<sub>2</sub>F<sub>3</sub>, NH<sub>3</sub>, N<sub>2</sub>H<sub>4</sub>, HCN, NO 2 − .</p></sec><sec id="s2_2"><title>2.2. Density ρ</title><p>It measures the sum of mass contained in a cubic meter of plasma and is mentioned in (kg∙m<sup>−3</sup>). It is calculated using the mass (kg) and the numerical density (m<sup>−3</sup>) of chemical species in the plasma [<xref ref-type="bibr" rid="scirp.125335-ref11">11</xref>] [<xref ref-type="bibr" rid="scirp.125335-ref13">13</xref>] [<xref ref-type="bibr" rid="scirp.125335-ref14">14</xref>] :</p><p>ρ = ∑ j = 1 N n j m j (1)</p><p>where n j and m j are the number density and mass of species j, respectively, and N is the number of species that constitute the plasma.</p></sec><sec id="s2_3"><title>2.3. Mass Enthalpy h</title><p>The mass enthalpy can be calculated by the following formula [<xref ref-type="bibr" rid="scirp.125335-ref17">17</xref>] :</p><p>h = 1 M ∑ i = 1 N X i ( h i 0 + e i 0 ) (2)</p><p>where h i 0 and e i 0 are the specific molar enthalpy and the enthalpy of formation of species i, respectively.</p></sec><sec id="s2_4"><title>2.4. Mass Heat at Constant Pressure C<sub>p</sub></title><p>It represents the capacity of a system to store heat. If the thermodynamic</p><table-wrap id="table1" ><label><xref ref-type="table" rid="table1">Table 1</xref></label><caption><title> Different plasmas studied</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Mixtures</th><th align="center" valign="middle" >Notation</th></tr></thead><tr><td align="center" valign="middle" >100% trifluoroethylamine</td><td align="center" valign="middle" >trif</td></tr><tr><td align="center" valign="middle" >100% nonafluoropentylamine.</td><td align="center" valign="middle" >nonaf</td></tr><tr><td align="center" valign="middle" >99% trif +1% air</td><td align="center" valign="middle" >Mix1</td></tr><tr><td align="center" valign="middle" >50% trif + 50% air</td><td align="center" valign="middle" >Mix50</td></tr><tr><td align="center" valign="middle" >99% nonaf + 1% air</td><td align="center" valign="middle" >Mix'1</td></tr><tr><td align="center" valign="middle" >50% nonaf + 50% air</td><td align="center" valign="middle" >Mix'50</td></tr></tbody></table></table-wrap><p>transformation of the system takes place at constant pressure, the specific heat can be calculated by [<xref ref-type="bibr" rid="scirp.125335-ref13">13</xref>] [<xref ref-type="bibr" rid="scirp.125335-ref14">14</xref>] [<xref ref-type="bibr" rid="scirp.125335-ref18">18</xref>] [<xref ref-type="bibr" rid="scirp.125335-ref19">19</xref>] :</p><p>C p = h T + Δ T − h T Δ T (3)</p><p>∆T is the temperature step.</p></sec><sec id="s2_5"><title>2.5. Sound Velocity in Plasma a</title><p>The speed of sound or sound velocity is the speed of propagation of waves in a fluid. It is defined as follows [<xref ref-type="bibr" rid="scirp.125335-ref20">20</xref>] [<xref ref-type="bibr" rid="scirp.125335-ref21">21</xref>] :</p><p>a = ( γ P ρ ) 1 / 2 (4)</p><p>where γ = C p C V , ρ the density, P the pressure in the plasma.</p></sec><sec id="s2_6"><title>2.6. Power Flow ϕ and Energy Density De</title><p>The power flow expresses the capacity plasma to evacuate energy to external environment. It is expressed by the following expression [<xref ref-type="bibr" rid="scirp.125335-ref13">13</xref>] [<xref ref-type="bibr" rid="scirp.125335-ref14">14</xref>] [<xref ref-type="bibr" rid="scirp.125335-ref16">16</xref>] [<xref ref-type="bibr" rid="scirp.125335-ref22">22</xref>] :</p><p>ϕ = ρ ⋅ h ⋅ a (5)</p><p>The energy density characterizes the distribution of energy in the specific environment. It is defined by the following expression [<xref ref-type="bibr" rid="scirp.125335-ref13">13</xref>] [<xref ref-type="bibr" rid="scirp.125335-ref14">14</xref>] [<xref ref-type="bibr" rid="scirp.125335-ref16">16</xref>] :</p><p>D e = ρ ⋅ h (6)</p></sec></sec><sec id="s3"><title>3. Results and Discussion</title><p>In this section, we present results of thermodynamic properties such as densities, enthalpies of mass, heats of mass at constant pressure, sound velocities, and others important parameters for plasma modeling such as energy densities and power flows in trifluoroethylamine and nonafluoropentylamine plasmas. Some results of the plasmas composition are briefly presented. The calculations were performed at atmospheric pressure and LTE.</p><p>We first compared our results from calculations density, mass enthalpy and heat capacity at constant pressure of the plasma formed of pure air with those of P. Andr&#233; [<xref ref-type="bibr" rid="scirp.125335-ref7">7</xref>] in Figures 1-3. We note that our results are in good agreement with those of P. Andr&#233;. We can note some differences. These differences could be due to the study methods and the data used.</p><sec id="s3_1"><title>3.1. Equilibrium Composition of Plasmas</title><p><xref ref-type="fig" rid="fig4">Figure 4</xref> and <xref ref-type="fig" rid="fig5">Figure 5</xref> show the equilibrium compositions of trifluoroethylamine (trif) and nonafluoropentylamine-air (mel'1) plasmas at LTE and atmospheric pressure (1 bar). We notice that, for temperatures beyond 15,000 K, molecular species completely disappear. Numerical densities of atomic species progressively decrease. Those of ions (C<sup>+</sup>, F<sup>+</sup>, H<sup>+</sup>, N<sup>+</sup>, O<sup>+</sup>) increase. It is also noticed that ions C<sup>2+</sup> and N<sup>2+</sup> appear.</p></sec><sec id="s3_2"><title>3.2. Mass Density</title><p>We have represented in <xref ref-type="fig" rid="fig6">Figure 6</xref> and <xref ref-type="fig" rid="fig7">Figure 7</xref> the evolution according to temperature of trifluoroethylamine (Trif), nonafluoropentylamine (Nonaf), trifluoroethylamine-air (Trif-Air) and nonafluoropentylamine-air (Nonaf-Air) plasmas volumic mass in atmospheric pressure and ETL. Regarding to these differents figures, the influence of the air percentage on the density of the trifluoroethylamine plasma is similar to its influence on that of the nonafluoropentylamine plasma. The density decreases with increase of temperature. The decrease following temperature is explained by the rarefaction effect linked to the</p><p>law of perfect gases and the dissociation, ionization of molecules progressively replaced at high temperatures by lighter atoms and electrons [<xref ref-type="bibr" rid="scirp.125335-ref23">23</xref>] . In other hand, it increases slightly with the percentage of air for temperatures less than 4500 K. Above this temperature, air has an almost negligible influence on the density. The increase with the percentage of air is not explained only by the increasment of species densities in the area but also by chemical reactions that take place.</p></sec><sec id="s3_3"><title>3.3. Mass Enthalpy</title><p><xref ref-type="fig" rid="fig8">Figure 8</xref> and <xref ref-type="fig" rid="fig9">Figure 9</xref> represent the variations of the mass enthalpies of the</p><p>trifluoroethylamine-air and nonafluoropentylamine-air mixture plasmas. The curves are plotted as a function of temperature, at LTE and at atmospheric pressure. These curves show similar evolutions. We find a well-known pattern in the literature, which is a continuous and increasing function of the temperature with shows some level of rapid evolution phases corresponding to the reactivity of the area and more particularly to the dissociation and ionization phenomena. This is highlighted by the variations of the heat capacity which depends strongly on the chemical reactions. The mass enthalpy varies lowly with the increase of air</p><p>percentage. However, a slight increase is observed at high temperature (T &gt; 14,000 K).</p></sec><sec id="s3_4"><title>3.4. Specific Heat</title><p><xref ref-type="fig" rid="fig10"><xref ref-type="fig" rid="fig1">Figure 1</xref>0</xref> and <xref ref-type="fig" rid="fig11"><xref ref-type="fig" rid="fig1">Figure 1</xref>1</xref> show the evolution, according to temperature, the heats of mass at constant pressure of trifluoroethylamine, nonafluoropentylamine, trifluoroethylamine-air and nonafluoropentylamine-air plasmas. These curves show quasi-similar evolutions, with the appearance of peaks. The comparison of these figures with <xref ref-type="fig" rid="fig1">Figure 1</xref> and <xref ref-type="fig" rid="fig2">Figure 2</xref> allows to associate the peaks of the heat capacities to chemical reactions. We observe more peaks in <xref ref-type="fig" rid="fig10"><xref ref-type="fig" rid="fig1">Figure 1</xref>0</xref></p><p>than in <xref ref-type="fig" rid="fig11"><xref ref-type="fig" rid="fig1">Figure 1</xref>1</xref>. The peaks appearing around a temperature of 1500 K corresponding to the dissociation of molecules C<sub>2</sub>H<sub>4</sub> and CH<sub>4</sub> (<xref ref-type="fig" rid="fig10"><xref ref-type="fig" rid="fig1">Figure 1</xref>0</xref>). The peaks appearing around 5000 K result from the dissociation of molecules (C<sub>2</sub>H<sub>2</sub>, C<sub>2</sub>F<sub>2</sub>) and radicals (C<sub>4</sub>N<sub>2</sub>, CH<sub>2</sub>, CH<sub>3</sub>, CF<sub>3</sub>) (<xref ref-type="fig" rid="fig10"><xref ref-type="fig" rid="fig1">Figure 1</xref>0</xref> and <xref ref-type="fig" rid="fig11"><xref ref-type="fig" rid="fig1">Figure 1</xref>1</xref>). The following peaks located around 7000 K correspond to the dissociation of molecules (HCN, F<sub>2</sub>) and radicals (C<sub>2</sub>F, CF<sub>2</sub>, C<sub>3</sub>, C<sub>2</sub>H). The following peaks located around 15,000 K correspond to the dissociation of molecules (HF, C<sub>2</sub>, N<sub>2</sub>), radicals (CF, CN, CH, CO) and the ionization of species such as (F, H, N, C, O, N<sup>+</sup>).</p></sec><sec id="s3_5"><title>3.5. Sound Velocity</title><p><xref ref-type="fig" rid="fig1">Figure 1</xref>2 and <xref ref-type="fig" rid="fig1">Figure 1</xref>3 represent the variation according to temperature, air percentage, the sound velocities in plasmas, trifluoroethylamine, nonafluoropentylamine, trifluoroethylamine-air and nonafluoropentylamine-air mixture. The sound speed in the plasma increases with temperature. In general, the sound velocity decreases slightly with the percentage of air for the Trifluoroethylamine-air mixture plasma. On other hand, the percentage of air has a negligible influence on the Nonafluoropentylamine-air mixture plasma.</p></sec><sec id="s3_6"><title>3.6. Energy Density</title><p><xref ref-type="fig" rid="fig1">Figure 1</xref>4 and <xref ref-type="fig" rid="fig1">Figure 1</xref>5 show air influence on energy densities of trifluoroethylamine, nonafluoropentylamine, trifluoroethylamine-air and nonafluoropentylamine-air plasmas. Between 500 K and 7000 K, the energy densities of trifluoroethylamine and nonafluoropentylamine plasmas decrease with the percentage of air in the mixture. They increase with the percentage of air for both plasmas between 7000 K and 20,000 K.</p></sec><sec id="s3_7"><title>3.7. Power Flow</title><p>To better appreciate the influence of air on plasmas power flows, we varied the</p><p>air content in the mixtures from 1% to 50%. <xref ref-type="fig" rid="fig1">Figure 1</xref>6 and <xref ref-type="fig" rid="fig1">Figure 1</xref>7 show the evolution of the power flows of the plasmas studied at atmospheric pressure and at LTE as a function of temperature. These power flows are important characteristics for the modelization of plasmas. Between 500 K and 7000 K, the power flow for trifluoroethylamine and nonafluoropentylamine plasmas decreases with the percentage of air in the mixture. The flow stay invariant with the percentage</p><p>of trifluoroethylamine plasma air between 7000 K and 20,000 K. In other hand, it slightly increases with the percentage of air for the nonafluoropentylamine plasma in the same temperature range.</p></sec></sec><sec id="s4"><title>4. Conclusion</title><p>In this paper, we have presented and analyzed the results of thermodynamic properties as well as parameters such as energy densities and power flows that are important for modeling thermal plasmas of trifluoroethylamine, nonafluoropentylamine, trifluoroethylamine-air and nonafluoropentylamine-air mixtures at local thermodynamic equilibrium and at atmospheric pressure. From the analysis, it appears that:</p><p>&#183; the density decreases with increasing temperature. In other hand, it increases slightly with the percentage of air for temperatures lower than 4500 K. Above this temperature, the densities are roughly equal;</p><p>&#183; the mass enthalpy shows a low variation with the increases of the percentage of air. However, a slight increase is observed at high temperature (T &gt; 14,000 K);</p><p>&#183; when the percentage of air increases, we observe a shift of the peaks of the specific heat of the plasma towards high temperatures and a slight decrease of their values. The comparison of <xref ref-type="fig" rid="fig10"><xref ref-type="fig" rid="fig1">Figure 1</xref>0</xref> and <xref ref-type="fig" rid="fig11"><xref ref-type="fig" rid="fig1">Figure 1</xref>1</xref>, with <xref ref-type="fig" rid="fig4">Figure 4</xref> and <xref ref-type="fig" rid="fig5">Figure 5</xref> allows to associate the peaks of the heat capacities to chemical reactions;</p><p>&#183; the sound speed in the plasma increases with temperature. But in general, the air percentage has practically an insignificant influence on the speed of sound in the plasma;</p><p>&#183; between 500 K and 7000 K, the energy densities of trifluoroethylamine and nonafluoropentylamine plasmas decrease with the percentage of air in the mixture. They increase with the percentage of air for both plasmas between 7000 K and 20,000 K;</p><p>&#183; between 500 K and 7000 K, the power flow for trifluoroethylamine and nonafluoropentylamine plasmas decreases with the percentage of air in the mixture. The flow stays invariant with the percentage of trifluoroethylamine plasma air between 7000 K and 20,000 K. In other hand, it slightly increases with the percentage of air for the nonafluoropentylamine plasma in the same temperature range.</p><p>The energy density and power flux results show that increasing percentage of air in the mixture can be even more interesting for the destruction of hazardous and toxic gaseous chemical species such as CF2, CO, HCN and HF which appear at low temperatures with high concentration.</p><p>We can therefore say that nonafluoropentylamine plasma performs better than trifluoroethylamine plasma.</p></sec><sec id="s5"><title>Conflicts of Interest</title><p>The authors declare no conflicts of interest regarding the publication of this paper.</p></sec><sec id="s6"><title>Cite this paper</title><p>Ibrahim, P., Ni&#232;ssan, K., Charles, Y.W., Karim, K.A., Zacharie, K. and Pascal, A. (2023) Study of the Thermodynamic Properties of Thermal Plasmas of Fluoroalkylamine-Air Mixtures. 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