<?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">MME</journal-id><journal-title-group><journal-title>Modern Mechanical Engineering</journal-title></journal-title-group><issn pub-type="epub">2164-0165</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/mme.2015.51001</article-id><article-id pub-id-type="publisher-id">MME-53766</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Engineering</subject></subj-group></article-categories><title-group><article-title>
 
 
  Stress Analysis of Thin-Walled Pressure Vessels
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>hmed</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>Yeong</surname><given-names>Ryu</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>Mir</surname><given-names>Saidpour</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib></contrib-group><aff id="aff1"><addr-line>Mechanical Engineering Technology, Farmingdale State College, Farmingdale, New York, USA</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>ahmed.ibrahim@farmingdale.edu(HI)</email>;<email>yeong.ryu@farmingdale.edu(YR)</email>;<email>mir.saidpour@farmingdale.edu(MS)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>03</day><month>02</month><year>2015</year></pub-date><volume>05</volume><issue>01</issue><fpage>1</fpage><lpage>9</lpage><history><date date-type="received"><day>15</day>	<month>January</month>	<year>2015</year></date><date date-type="rev-recd"><day>accepted</day>	<month>1</month>	<year>February</year>	</date><date date-type="accepted"><day>3</day>	<month>February</month>	<year>2015</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><html>
 <head></head>
 
  This paper discusses the stresses developed in a thin-walled pressure vessels. Pressure vessels (cylindrical or spherical) are designed to hold gases or liquids at a pressure substantially higher than the ambient pressure. Equations of static equilibrium along with the free body diagrams will be used to determine the normal stresses 
  <img src="Edit_6743896e-40c3-4b82-89c3-8e83a309735a.bmp" alt="" /> in the circumferential or hoop direction and
  <img src="Edit_78a8aa44-0279-4af6-9a6c-f13e89beb26c.bmp" alt="" /> in the longitudinal or axial direction. A case study of internal pressure developed in a soda can was determined by measuring the elastic strains of the surface of the soda can through strain gages attached to the can and connected to Strain indicator Vishay model 3800.
 
</html></p></abstract><kwd-group><kwd>Stress Analysis</kwd><kwd> Thin-Walled Pressure Vessel</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Pressure vessels are compressed gas storage tanks designed to hold gases or liquids at a pressure substantially different from the ambient pressure. They have a variety of applications in industry, including in oil refineries, nuclear reactors, gas reservoirs, etc. An aircraft fuselage, a gas cylinder and a soda can, all are pressure vessels which must be designed to meet very specific requirements of integrity. The human arteries maintain pressure in the circulatory system much like a balloon maintains pressure on the air within it. The arteries therefore act as pressure vessels by maintaining pressure. Pressure vessels can be any shape, but shapes made of sections of spheres and cylinders are usually employed. A common design is a cylinder with end caps called heads. Head shapes are frequently hemispherical.</p><p>Cracked or damaged vessels can result in leakage or rupture failures. Potential health and safety hazards of leaking vessels include poisonings, suffocations, fires, and explosion hazards. Rupture failures can be much more catastrophic and can cause considerable damage to life and property. The safe design, installation, operation, and maintenance of pressure vessels are in accordance with codes such as American Society of Mechanical Engineers (ASME) boiler and pressure vessel code [<xref ref-type="bibr" rid="scirp.53766-ref1">1</xref>] . Therefore, great emphasis should be placed on analytical and experimental methods for determining their operating stresses.</p><p>Spherical Pressure Vessel, like the one shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>, is preferred for storage of high pressure fluids. A spherical pressure vessel has approximately twice the strength of a cylindrical pressure vessel with the same wall thickness. A sphere is a very strong structure. The distribution of stresses on the sphere’s surfaces, both internally and externally are equal. Spheres however, are much more costly to manufacture than cylindrical vessels. A spherical storage has a smaller surface area per unit volume than any other shape of vessel. This means, that the quantity of heat transferred from warmer surroundings to the liquid in the sphere, will be less than that for cylindrical storage vessels.</p><p>Pressure vessels are subjected to tensile forces within the walls of the container. The normal stress in the walls of the container is proportional to the pressure and radius of the vessel and inversely proportional to the thickness of the walls [<xref ref-type="bibr" rid="scirp.53766-ref2">2</xref>] [<xref ref-type="bibr" rid="scirp.53766-ref3">3</xref>] . As a general rule, pressure vessels are considered to be thin-walled when the ratio of radius r to wall thickness t is greater than 10 [<xref ref-type="bibr" rid="scirp.53766-ref4">4</xref>] . Pressure vessels fail when the stress state in the wall exceeds some failure criterion [<xref ref-type="bibr" rid="scirp.53766-ref5">5</xref>] [<xref ref-type="bibr" rid="scirp.53766-ref6">6</xref>] . Therefore pressure vessels are designed to have a thickness proportional to the radius of tank and the pressure of the tank and inversely proportional to the maximum allowed normal stress of the particular material used in the walls of the container. Thus, it is important to understand and quantify (analyze) stresses in pressure vessels. In this paper we will analyze the stresses in thin-walled pressure vessels (cylindrical &amp; spherical shapes), like the one shown in <xref ref-type="fig" rid="fig1">Figure 1</xref> &amp; <xref ref-type="fig" rid="fig2">Figure 2</xref>. In addition, a case study of internal stresses developed in a soda can will be presented and discussed.</p><fig id="fig1"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> Japanese gas companies added a touch of character to giant spherical gas tanks</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-1860230x8.png"/></fig><fig id="fig2"  position="float"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> Cylindrical pressure vessel in a chemical plant</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-1860230x9.png"/></fig></sec><sec id="s2"><title>2. Thin-Walled-Cylindrical Pressure Vessel</title><p>A thin-walled circular tank AB subjected to internal pressure shown in <xref ref-type="fig" rid="fig3">Figure 3</xref>. A stress element with its faces parallel and perpendicular to the axis of the tank is shown on the wall of the tank. The normal stresses <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x10.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x11.png" xlink:type="simple"/></inline-formula> acting on the side faces of this element. No shear stresses act on these faces because of the symmetry of the vessel and its loading. Therefore, the stresses <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x12.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x13.png" xlink:type="simple"/></inline-formula><sub> </sub>are principal stresses. Because of their directions, the stress <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x14.png" xlink:type="simple"/></inline-formula> is called the circumferential stress or the hoop stress, and the stress <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x15.png" xlink:type="simple"/></inline-formula><sub> </sub>is called the longitudinal stress or the axial stress. Each of these stresses can be calculated from static equilibrium equations.</p><p>Several assumptions have been made to derive the following equations for circumferential and longitudinal stresses:</p><p>1) Plane sections remain plane</p><p>2) <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x16.png" xlink:type="simple"/></inline-formula>with <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x17.png" xlink:type="simple"/></inline-formula> being uniform and constant</p><p>3) Material is linear-elastic, isotropic and homogeneous.</p><p>4) Stress distributions throughout the wall thickness will not vary</p><p>5) Weight of the fluid is considered negligible.</p></sec><sec id="s3"><title>3. Circumferential Stress</title><p>To determine the circumferential stress<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x18.png" xlink:type="simple"/></inline-formula>, make three sections (cd and ef) perpendicular to the longitudinal axis and distance <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x19.png" xlink:type="simple"/></inline-formula> apart (<xref ref-type="fig" rid="fig3">Figure 3</xref>(a)); and a third cut in a vertical plane through the longitudinal axis of the tank. The resulting free body diagram is shown in <xref ref-type="fig" rid="fig3">Figure 3</xref>(b). Acting on the longitudinal cut (plane cefd) are the circumferential stresses <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x20.png" xlink:type="simple"/></inline-formula> and the internal pressure<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x21.png" xlink:type="simple"/></inline-formula>.</p><p>The circumferential stresses <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x22.png" xlink:type="simple"/></inline-formula> acting in the wall of the vessel have a resultant equal to<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x23.png" xlink:type="simple"/></inline-formula>, where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x24.png" xlink:type="simple"/></inline-formula> is the thickness of the wall. Also, the resultant force <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x24.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x25.png" xlink:type="simple"/></inline-formula> of the internal pressure is equal to<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x24.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x25.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x26.png" xlink:type="simple"/></inline-formula>, where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x24.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x25.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x26.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x27.png" xlink:type="simple"/></inline-formula> is the inner radius of the cylinder. Hence, we have the following equation of equilibrium:</p><disp-formula id="scirp.53766-formula33"><graphic  xlink:href="http://html.scirp.org/file/1-1860230x28.png"  xlink:type="simple"/></disp-formula><p>From the above equation, the circumferential stress in a pressurized cylinder can be found:</p><fig id="fig3"  position="float"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> Stresses in a circular cylindrical presure vessel</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-1860230x29.png"/></fig><disp-formula id="scirp.53766-formula34"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-1860230x30.png"  xlink:type="simple"/></disp-formula><p>If there exist an external pressure <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x31.png" xlink:type="simple"/></inline-formula> and an internal pressure<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x32.png" xlink:type="simple"/></inline-formula>, the formula may be expressed as:</p><disp-formula id="scirp.53766-formula35"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-1860230x33.png"  xlink:type="simple"/></disp-formula></sec><sec id="s4"><title>4. Longitudinal Stress</title><p>The longitudinal stress <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x34.png" xlink:type="simple"/></inline-formula> is obtained from the equilibrium of a free body diagram shown in <xref ref-type="fig" rid="fig3">Figure 3</xref>(c). The stresses <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x34.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x35.png" xlink:type="simple"/></inline-formula><sub> </sub>acts longitudinally and have a resultant force equal to <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x34.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x35.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x36.png" xlink:type="simple"/></inline-formula> <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x34.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x35.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x36.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x37.png" xlink:type="simple"/></inline-formula>. The resultant force <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x34.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x35.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x36.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x37.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x38.png" xlink:type="simple"/></inline-formula> of the internal pressure is a force equal to<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x34.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x35.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x36.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x37.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x38.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x39.png" xlink:type="simple"/></inline-formula>. The equation of equilibrium for the free body diagram is</p><disp-formula id="scirp.53766-formula36"><graphic  xlink:href="http://html.scirp.org/file/1-1860230x40.png"  xlink:type="simple"/></disp-formula><p>Solving the above equation for<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x41.png" xlink:type="simple"/></inline-formula>, lead to the following formula for the longitudinal stress in a cylindrical pressure vessel:</p><disp-formula id="scirp.53766-formula37"><label>(3)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-1860230x42.png"  xlink:type="simple"/></disp-formula><p>If there exist an external pressure <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x43.png" xlink:type="simple"/></inline-formula> and an internal pressure<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x43.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x44.png" xlink:type="simple"/></inline-formula>, the formula may be expressed as:</p><disp-formula id="scirp.53766-formula38"><label>(4)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-1860230x45.png"  xlink:type="simple"/></disp-formula><p>Comparing Equations (1) and (3) we find that the circumferential stress in a cylindrical vessel is equal to twice the longitudinal stress:</p><disp-formula id="scirp.53766-formula39"><label>(5)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-1860230x46.png"  xlink:type="simple"/></disp-formula><p>Due to this, cylindrical pressure vessels will split on the wall instead of being pulled apart like it would under an axial load.</p></sec><sec id="s5"><title>5. Stresses at the Outer Surface</title><p>The principal stresses <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x47.png" xlink:type="simple"/></inline-formula>and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x47.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x48.png" xlink:type="simple"/></inline-formula> at the outer surface of a cylindrical vessel are shown on the stress element of <xref ref-type="fig" rid="fig4">Figure 4</xref>(a). The element is in biaxial stress (stress in z direction is zero).</p><p>The maximum in-plane shear stresses occur on planes that are rotated 45˚ about the z axis:</p><disp-formula id="scirp.53766-formula40"><graphic  xlink:href="http://html.scirp.org/file/1-1860230x49.png"  xlink:type="simple"/></disp-formula><p>The maximum out-of-plane shear stresses occur on planes that are rotated 45˚ about <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x50.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x50.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x51.png" xlink:type="simple"/></inline-formula> axes, respectively:</p><disp-formula id="scirp.53766-formula41"><graphic  xlink:href="http://html.scirp.org/file/1-1860230x52.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.53766-formula42"><graphic  xlink:href="http://html.scirp.org/file/1-1860230x53.png"  xlink:type="simple"/></disp-formula><p>Therefore, the maximum absolute shear stress is:</p><disp-formula id="scirp.53766-formula43"><label>(6)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-1860230x54.png"  xlink:type="simple"/></disp-formula><p>Occurs on a plane rotated by 45˚ about the x-axis.</p></sec><sec id="s6"><title>6. Stresses at the Inner Surface</title><p>The stress conditions at the inner surface of the wall of the vessel are shown in <xref ref-type="fig" rid="fig4">Figure 4</xref>(b). The principal stresses</p><fig id="fig4"  position="float"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> Stresses in a circular cylindrical pressure vessel at (a) the outer surface, (b) the inner surface</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-1860230x55.png"/></fig><p>are:</p><disp-formula id="scirp.53766-formula44"><graphic  xlink:href="http://html.scirp.org/file/1-1860230x56.png"  xlink:type="simple"/></disp-formula><p>The three maximum shear stresses, obtained by 45˚ rotations about the<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x57.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x57.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x58.png" xlink:type="simple"/></inline-formula>, and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x57.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x58.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x59.png" xlink:type="simple"/></inline-formula> axes, are</p><disp-formula id="scirp.53766-formula45"><label>(7)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-1860230x60.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.53766-formula46"><label>(8)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-1860230x61.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.53766-formula47"><label>(9)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-1860230x62.png"  xlink:type="simple"/></disp-formula><p>When <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x63.png" xlink:type="simple"/></inline-formula> is very large (thin walled), the term <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x63.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x64.png" xlink:type="simple"/></inline-formula> can be disregarded, and the equations are the same as the stresses at the outer.</p></sec><sec id="s7"><title>7. Spherical Pressure Vessel</title><p>A similar approach can be used to derive an expression for an internally pressurized thin-wall spherical vessel. A spherical pressure vessel is just a special case of a cylindrical vessel.</p><p>To find <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x65.png" xlink:type="simple"/></inline-formula> we cut the sphere into two hemispheres as shown in <xref ref-type="fig" rid="fig5">Figure 5</xref>. The free-body diagram gives the equilibrium condition<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x65.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x66.png" xlink:type="simple"/></inline-formula>, hence</p><disp-formula id="scirp.53766-formula48"><label>(10)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-1860230x67.png"  xlink:type="simple"/></disp-formula><p>Any section that passes through the center of the sphere yields the same result. Comparing Equations (1), (3), and (10) yields that for the same<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x68.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x68.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x69.png" xlink:type="simple"/></inline-formula>and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x68.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x69.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x70.png" xlink:type="simple"/></inline-formula> the spherical geometry is twice as efficient in terms of wall stress.</p><p>As shown in <xref ref-type="fig" rid="fig6">Figure 6</xref>, the internal pressure of the cylindrical vessel is resisted by the hoop stress in “arch action” whereas the axial stress does not contribute. In the spherical vessel the double curvature means that all stress directions around the pressure point contribute to resisting the pressure.</p><fig id="fig5"  position="float"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> Stresses in a spherical pressure vessel</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-1860230x71.png"/></fig><fig id="fig6"  position="float"><label><xref ref-type="fig" rid="fig6">Figure 6</xref></label><caption><title> (a) Spherical pressure vessel; (b) Cylindrical pressure vessel</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-1860230x72.png"/></fig></sec><sec id="s8"><title>8. Case Study: Measuring Internal Pressure in a Soda Can Using Strain Gauges</title><p>The soda can is analyzed as a thin wall pressure vessel. In a thin wall pressure vessel, two stresses exist: the longitudinal stress <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x73.png" xlink:type="simple"/></inline-formula> and the hoop stress <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x73.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x74.png" xlink:type="simple"/></inline-formula> (<xref ref-type="fig" rid="fig7">Figure 7</xref>). The longitudinal stress is a result of the internal pressure acting on the ends of the cylinder and stretching the length of the cylinder as shown in <xref ref-type="fig" rid="fig8">Figure 8</xref>. The hoop stress is the result of the radial action of the internal pressure that tends to increase the circumference of the can.</p><p>The pressure developed in a soda can be determined by measuring the elastic strains of the surface of the soda can. Internal pressure for a pressurized soda can be derived using basic Hooke’s law stress and strain relations that relate change in hoop and axial strains to internal pressure. Two strain gauges (Measurements Group-CEA series gages) was attached to the soda can (<xref ref-type="fig" rid="fig9">Figure 9</xref>) to measure the change in strains, as measured through the voltage across a calibrated Wheatstone bridge. M-bond 200 adhesive (Measurements Group, Inc) was used to glue the strain gages to the surface of the soda can.</p><p>The hoop stress for the thin walled cylinder can be calculated from Equation (1)</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x75.png" xlink:type="simple"/></inline-formula>where:</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x76.png" xlink:type="simple"/></inline-formula>―internal pressure (psi)</p><p>D―mean diameter of cylinder (in.)</p><p>t―wall thickness (in.)</p><p>Similarly, the longitudinal stress cylinder wall can be calculated from Equation (3)</p><disp-formula id="scirp.53766-formula49"><graphic  xlink:href="http://html.scirp.org/file/1-1860230x77.png"  xlink:type="simple"/></disp-formula><p>Equation (5) yields</p><disp-formula id="scirp.53766-formula50"><graphic  xlink:href="http://html.scirp.org/file/1-1860230x78.png"  xlink:type="simple"/></disp-formula><fig id="fig7"  position="float"><label><xref ref-type="fig" rid="fig7">Figure 7</xref></label><caption><title> Coca cola soda can</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-1860230x79.png"/></fig><fig id="fig8"  position="float"><label><xref ref-type="fig" rid="fig8">Figure 8</xref></label><caption><title> Longitudinal stress distribution</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-1860230x80.png"/></fig><fig id="fig9"  position="float"><label><xref ref-type="fig" rid="fig9">Figure 9</xref></label><caption><title> Strain gages attached to a soda can and strain indicator vishay model 3800</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-1860230x81.png"/></fig><p>Assuming that:</p><p>・ The material is homogeneous and isotropic,</p><p>・ The can is loaded only within its elastic range,</p><p>・ A biaxial state of stress exists in the can,</p><p>The internal stresses developed in the soda can are proportional to the elastic strains of the outside surface of the soda can as follow:</p><disp-formula id="scirp.53766-formula51"><label>(11)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-1860230x82.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.53766-formula52"><label>(12)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-1860230x83.png"  xlink:type="simple"/></disp-formula><p>where:</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x84.png" xlink:type="simple"/></inline-formula>―modulus of elasticity or Young’s modulus (psi)</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x85.png" xlink:type="simple"/></inline-formula>―Poisson’s ratio</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x86.png" xlink:type="simple"/></inline-formula>―hoop strain (in/in)</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x87.png" xlink:type="simple"/></inline-formula>―longitudinal strain (in/in)</p><p>Using Equations (11) and (12) with Equation (5), and simplifying results in:</p><disp-formula id="scirp.53766-formula53"><label>(13)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-1860230x88.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.53766-formula54"><label>(14)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-1860230x89.png"  xlink:type="simple"/></disp-formula><p>Thus the pressure can be calculated directly from the measured strains by substituting Equations (13) and (14) back into Equation (1) and (2) to get:</p><disp-formula id="scirp.53766-formula55"><label>(15)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-1860230x90.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.53766-formula56"><label>(16)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-1860230x91.png"  xlink:type="simple"/></disp-formula><p>Once we have Equations (15) and (16), then the internal pressure in the can may be directly calculated from the measured longitudinal and hoop strains.</p></sec><sec id="s9"><title>9. Internal Pressure Results</title><p>Measured Values</p><p>Can thickness: t = 0.004 in</p><p>Can diameter: D = 2.59 in</p><p>Young’s Modulus: E = 10 &#215; 106 psi (assumed)</p><p>Poisson’s Ratio: <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x92.png" xlink:type="simple"/></inline-formula></p><p>The change in longitudinal and hoop strains were measured after the pressure was released from the cans. The results of the strains and corresponding pressures are shown in <xref ref-type="table" rid="table1">Table 1</xref>.</p></sec><sec id="s10"><title>10. Conclusion</title><p>This paper presented a detailed stress analysis of the stresses developed in thin-walled pressure vessels (cylindrical &amp; spherical). Then, a case study of a soda can that was analyzed as a thin wall pressure vessel was discussed. The elastic strains (<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x93.png" xlink:type="simple"/></inline-formula>&amp;<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x93.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x94.png" xlink:type="simple"/></inline-formula>) of the external surface of the soda can was determined through strain gages attached to the can surface and connected to a strain indicator. The longitudinal stress, hoop stress, and the internal pressure were determined from equations of generalized Hooke’s law for stress and strain. Small varia-</p><table-wrap id="table1" ><label><xref ref-type="table" rid="table1">Table 1</xref></label><caption><title> Elastic strains and corresponding internal pressures in a Soda can</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Test</th><th align="center" valign="middle" ></th><th align="center" valign="middle" >Strain &#215; 10<sup>−6</sup> in/in</th><th align="center" valign="middle" >Internal Pressure (psi)</th></tr></thead><tr><td align="center" valign="middle"  rowspan="2"  >1</td><td align="center" valign="middle" >Longitudinal</td><td align="center" valign="middle" >−275</td><td align="center" valign="middle" >−42.5</td></tr><tr><td align="center" valign="middle" >Hoop</td><td align="center" valign="middle" >−1248</td><td align="center" valign="middle" >−45.4</td></tr><tr><td align="center" valign="middle"  rowspan="2"  >2</td><td align="center" valign="middle" >Longitudinal</td><td align="center" valign="middle" >−295</td><td align="center" valign="middle" >−45.6</td></tr><tr><td align="center" valign="middle" >Hoop</td><td align="center" valign="middle" >−1172</td><td align="center" valign="middle" >−42.2</td></tr><tr><td align="center" valign="middle"  rowspan="2"  >3</td><td align="center" valign="middle" >Longitudinal</td><td align="center" valign="middle" >−224</td><td align="center" valign="middle" >−41.3</td></tr><tr><td align="center" valign="middle" >Hoop</td><td align="center" valign="middle" >−1156</td><td align="center" valign="middle" >−42</td></tr></tbody></table></table-wrap><p>tions recorded in internal pressures calculated from the longitudinal strain <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x95.png" xlink:type="simple"/></inline-formula> and the hoop strain<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x95.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-1860230x96.png" xlink:type="simple"/></inline-formula>.</p></sec><sec id="s11"><title>NOTES</title></sec></body><back><ref-list><title>References</title><ref id="scirp.53766-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Rao, K. 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