<?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">APM</journal-id><journal-title-group><journal-title>Advances in Pure Mathematics</journal-title></journal-title-group><issn pub-type="epub">2160-0368</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/apm.2015.510057</article-id><article-id pub-id-type="publisher-id">APM-58869</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Physics&amp;Mathematics</subject></subj-group></article-categories><title-group><article-title>
 
 
  Asymptotically Confirmed Hypotheses Method for the Construction of Micropolar and Classical Theories of Elastic Thin Shells
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>amvel</surname><given-names>Sargsyan</given-names></name><xref ref-type="aff" rid="aff1"><sub>1</sub></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib></contrib-group><aff id="aff1"><label>1</label><addr-line>Department of Physical Mathematical Sciences, Gyumri State Pedagogical Institute, Gyumri, Armenia</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>s_sargsyan@yahoo.com</email></corresp></author-notes><pub-date pub-type="epub"><day>12</day><month>08</month><year>2015</year></pub-date><volume>05</volume><issue>10</issue><fpage>629</fpage><lpage>642</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>16</month>	<year>August</year>	</date><date date-type="accepted"><day>19</day>	<month>August</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>
 
 
  In the present paper asymptotic solution of boundary-value problem of three-dimensional micropolar theory of elasticity with free fields of displacements and rotations is constructed in thin domain of the shell. This boundary-value problem is singularly perturbed with small geometric parameter. Internal iteration process and boundary layers are constructed, problem of their jointing is studied and boundary conditions for each of them are obtained. On the basis of the results of the internal boundary-value problem the asymptotic two-dimensional model of micropolar elastic thin shells is constructed. Further, the qualitative aspects of the asymptotic solution are accepted as hypotheses and on the basis of them general applied theory of micropolar elastic thin shells is constructed. It is shown that both the constructed general applied theory of micropolar elastic thin shells and the classical theory of elastic thin shells with consideration of transverse shear deformations are asymptotically confirmed theories.
 
</p></abstract><kwd-group><kwd>Micropolar</kwd><kwd> Elastic</kwd><kwd> Thin Shell</kwd><kwd> Asymptotic Model</kwd><kwd> Applied Theory</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Current methods of reducing three-dimensional problem of theory of elasticity to two-dimensional problem of theory of plates and shells are the followings: 1) hypotheses method; 2) method of expansion by thickness; 3) asymptotic method [<xref ref-type="bibr" rid="scirp.58869-ref1">1</xref>] -[<xref ref-type="bibr" rid="scirp.58869-ref9">9</xref>] . From recent important papers on construction of micropolar elastic thin plates and shells must be noted papers [<xref ref-type="bibr" rid="scirp.58869-ref10">10</xref>] [<xref ref-type="bibr" rid="scirp.58869-ref11">11</xref>] , where also review of researches is done in the mentioned direction.</p><p>The main problem of the general theory of micropolar or classical elastic thin plates and shells is in approximate, but adequate reduction of three-dimensional boundary-value problem of the micropolar or classical theory of elasticity to two-dimensional problem. From our point of view, for achievement of this aim [<xref ref-type="bibr" rid="scirp.58869-ref12">12</xref>] -[<xref ref-type="bibr" rid="scirp.58869-ref14">14</xref>] during the construction of applied theories of thin plates and shells main results of the asymptotic solution of boundary-value or initial boundary-value problem of three-dimensional micropolar or classical theory of elasticity in corresponding thin domains can be used, which are formulated as hypotheses [<xref ref-type="bibr" rid="scirp.58869-ref15">15</xref>] -[<xref ref-type="bibr" rid="scirp.58869-ref18">18</xref>] . Micropolar and classical theories of elastic thin plates and shells, constructed on the basis of such approach, are asymptotically correct theories. This problem is also essential in classical theory of elasticity during the construction of mathematical models of thin plates and shells with the account of transverse shear deformations: in paper [<xref ref-type="bibr" rid="scirp.58869-ref19">19</xref>] it is shown that one of the main theories of plates and shells of Timoshenko’s type, where transverse shear deformations are taken into account, is not asymptotically consistent.</p></sec><sec id="s2"><title>2. Problem Statement</title><p>A shell of constant thickness 2h is considered as a three-dimensional elastic body. Equations of the static problem of asymmetric (micropolar, momental) theory of elasticity with free fields of displacements and rotations are the followings [<xref ref-type="bibr" rid="scirp.58869-ref20">20</xref>] [<xref ref-type="bibr" rid="scirp.58869-ref21">21</xref>] :</p><p>Equilibrium equations:</p><disp-formula id="scirp.58869-formula896"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x5.png"  xlink:type="simple"/></disp-formula><p>Physical relations:</p><disp-formula id="scirp.58869-formula897"><label>. (2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x6.png"  xlink:type="simple"/></disp-formula><p>Geometrical relations:</p><disp-formula id="scirp.58869-formula898"><label>. (3)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x7.png"  xlink:type="simple"/></disp-formula><p>Here <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x8.png" xlink:type="simple"/></inline-formula> are the components of tensors of force and moment stresses; <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x9.png" xlink:type="simple"/></inline-formula>are the components of tensors of deformation and bending-torsion; <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x10.png" xlink:type="simple"/></inline-formula>are the components of displacement vector; <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x11.png" xlink:type="simple"/></inline-formula>are the components of free rotation; <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x12.png" xlink:type="simple"/></inline-formula>are physical constants of the micropolar material of the shell; indices <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x13.png" xlink:type="simple"/></inline-formula> take values 1, 2, 3.</p><p>It should be noted that if<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x14.png" xlink:type="simple"/></inline-formula>, main equations of the classical theory of elasticity will be obtained from Equations (1)-(3).</p><p>We’ll consider three orthogonal system of coordinates <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x15.png" xlink:type="simple"/></inline-formula> (<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x16.png" xlink:type="simple"/></inline-formula>,<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x17.png" xlink:type="simple"/></inline-formula>), accepted in theory of shells [<xref ref-type="bibr" rid="scirp.58869-ref4">4</xref>] .</p><p>Boundary conditions of the first boundary-value problem for front surfaces of the shell are accepted:</p><disp-formula id="scirp.58869-formula899"><label>(4)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x18.png"  xlink:type="simple"/></disp-formula><p>Boundary conditions on the edge <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x19.png" xlink:type="simple"/></inline-formula> of the shell are boundary conditions of the mixed boundary- value problem:</p><disp-formula id="scirp.58869-formula900"><label>(5)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x20.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x21.png" xlink:type="simple"/></inline-formula> are the components of the given loads and moments on<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x22.png" xlink:type="simple"/></inline-formula>;<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x23.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x24.png" xlink:type="simple"/></inline-formula>are the given components of displacement and free rotation vectors on<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x22.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x23.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x24.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x25.png" xlink:type="simple"/></inline-formula>.</p></sec><sec id="s3"><title>3. Asymptotic Solution (Construction of Internal Problem) of Boundary-Value Problem of Three-Dimensional Micropolar Theory of Elasticity in Thin Domain of the Shell</title><p>It is assumed that the thickness 2h of the shell is small compared with typical radius of curvature of the middle surface of the shell<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x26.png" xlink:type="simple"/></inline-formula>. We’ll proceed from the following basic concept [<xref ref-type="bibr" rid="scirp.58869-ref4">4</xref>] : in the static case general stress-strain state (SSS) of thin shell is composed of internal SSS, covering all three-dimensional shell, and boundary layers, localizing near the surface of the shell edge<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x26.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x27.png" xlink:type="simple"/></inline-formula>. On the basis of such approach and results of initial approximation of internal problem the construction of general two-dimensional (asymptotic) model of micropolar thin shells will be possible (in case of <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x26.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x27.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x28.png" xlink:type="simple"/></inline-formula> also model of elastic shell by classical theory of elasticity).</p><p>Question of reduction of three-dimensional static problem of asymmetric theory of elasticity for thin domain of the shell to two-dimensional problem is considered on the basis of asymptotic method with boundary layer [<xref ref-type="bibr" rid="scirp.58869-ref14">14</xref>] , including the question of satisfaction of boundary conditions on shell edge<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x29.png" xlink:type="simple"/></inline-formula>.</p><p>At first we’ll consider the construction of internal interactive process. For achievement of this aim we’ll pass to dimensionless coordinates in three-dimensional Equations (1)-(3) of asymmetric theory of elasticity:</p><disp-formula id="scirp.58869-formula901"><label>(6)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x30.png"  xlink:type="simple"/></disp-formula><p>Here quantity <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x31.png" xlink:type="simple"/></inline-formula> characterizes the variability of SSS by coordinates; p, l are integers,<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x32.png" xlink:type="simple"/></inline-formula>; R is the characteristic radius of curvature of the shell middle surface; <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x32.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x33.png" xlink:type="simple"/></inline-formula>is the big constant dimensionless geometric parameter, determined with the help of formula<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x32.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x33.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x34.png" xlink:type="simple"/></inline-formula>. Following dimensionless quantities and dimensionless physical parameters are also considered:</p><disp-formula id="scirp.58869-formula902"><label>(7)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x35.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.58869-formula903"><label>. (8)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x36.png"  xlink:type="simple"/></disp-formula><p>On the basis of (7), (8) following system of dimensionless equations will be obtained instead of system of Equations (1)-(3).</p><p>Equilibrium equations:</p><disp-formula id="scirp.58869-formula904"><label>(9)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x37.png"  xlink:type="simple"/></disp-formula><p>Physical-geometrical relations:</p><disp-formula id="scirp.58869-formula905"><label>(10)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x38.png"  xlink:type="simple"/></disp-formula><p>Here</p><disp-formula id="scirp.58869-formula906"><label>(11)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x39.png"  xlink:type="simple"/></disp-formula><p>The case is considered when dimensionless physical parameters (8) have the following values:</p><disp-formula id="scirp.58869-formula907"><label>(12)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x40.png"  xlink:type="simple"/></disp-formula><p>Following replacements of unknown quantities will be done:</p><disp-formula id="scirp.58869-formula908"><label>(13)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x41.png"  xlink:type="simple"/></disp-formula><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x42.png" xlink:type="simple"/></inline-formula>at at</p><p>As a result following system of equations will be obtained:</p><disp-formula id="scirp.58869-formula909"><label>(14)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x45.png"  xlink:type="simple"/></disp-formula><p>where</p><disp-formula id="scirp.58869-formula910"><label>(15)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x46.png"  xlink:type="simple"/></disp-formula><p>Following to the asymptotic method, the question is the following: to reduce three-dimensional Equations (14) (with free variables<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x47.png" xlink:type="simple"/></inline-formula>) to two-dimensional ones (with free variables<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x47.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x48.png" xlink:type="simple"/></inline-formula>).</p><p>Following formulas will be obtained for displacements and rotations, force and moment stresses with asymptotic accuracy <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x49.png" xlink:type="simple"/></inline-formula> on the basis of system (14):</p><disp-formula id="scirp.58869-formula911"><label>(16)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x50.png"  xlink:type="simple"/></disp-formula><p>where</p><disp-formula id="scirp.58869-formula912"><graphic  xlink:href="http://html.scirp.org/file/3-5300790x51.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.58869-formula913"><label>(17)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x52.png"  xlink:type="simple"/></disp-formula><p>The aim is to construct asymptotically strictly interactive process for averaged along the shell thickness quantities, which determine the stated problem (i.e. depending only on quantities<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x53.png" xlink:type="simple"/></inline-formula>). From this point of view there is an opportunity to define values from (16) of force stress <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x53.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x54.png" xlink:type="simple"/></inline-formula> and moment stress<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x53.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x54.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x55.png" xlink:type="simple"/></inline-formula>. The approach is the following: at the level of initial approximation of the asymptotic method for quantities <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x53.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x54.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x55.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x56.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x53.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x54.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x55.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x56.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x57.png" xlink:type="simple"/></inline-formula> we have:</p><disp-formula id="scirp.58869-formula914"><label>(18)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x58.png"  xlink:type="simple"/></disp-formula><p>Keeping quantities up to <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x59.png" xlink:type="simple"/></inline-formula> order in equilibrium equations and integrating these equations by<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x59.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x60.png" xlink:type="simple"/></inline-formula>, we’ll obtain:</p><disp-formula id="scirp.58869-formula915"><label>(19)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x61.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.58869-formula916"><label>(20)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x62.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x63.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x63.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x64.png" xlink:type="simple"/></inline-formula> are constants of the integration:</p><disp-formula id="scirp.58869-formula917"><label>(21)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x65.png"  xlink:type="simple"/></disp-formula><p>It must be required that averaged values along the shell thickness of quantities <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x66.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x66.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x67.png" xlink:type="simple"/></inline-formula> are equal to zero:</p><disp-formula id="scirp.58869-formula918"><label>(22)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x68.png"  xlink:type="simple"/></disp-formula><p>Substituting (19) and (20) into conditions (22), following formulas will be obtained for <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x69.png" xlink:type="simple"/></inline-formula> and<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x69.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x70.png" xlink:type="simple"/></inline-formula>:</p><disp-formula id="scirp.58869-formula919"><graphic  xlink:href="http://html.scirp.org/file/3-5300790x71.png"  xlink:type="simple"/></disp-formula><p>Thus for <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x72.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x72.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x73.png" xlink:type="simple"/></inline-formula> we’ll obtain:</p><disp-formula id="scirp.58869-formula920"><label>(23)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x74.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.58869-formula921"><label>(24)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x75.png"  xlink:type="simple"/></disp-formula><p>Finally, for quantities <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x76.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x76.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x77.png" xlink:type="simple"/></inline-formula> we’ll have the sum of (18), (23), (24):</p><disp-formula id="scirp.58869-formula922"><label>(25)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x78.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.58869-formula923"><label>(26)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x79.png"  xlink:type="simple"/></disp-formula><p>It should be noted that averaged along the shell thickness quantities for <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x80.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x80.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x81.png" xlink:type="simple"/></inline-formula> at the level (18) and (25), (26) are equal.</p><p>Thus, taking into consideration (25), (26), we’ll have following formulas for displacements, rotations, force and moment stresses instead of (16):</p><disp-formula id="scirp.58869-formula924"><label>(27)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x82.png"  xlink:type="simple"/></disp-formula><p>The constructed asymptotics (27) for internal interaction process of the stated problem gives an opportunity to reduce three-dimensional problem to two-dimensional one (what is already done for displacements, rotations, force and moment stresses). As in the classical theory, instead of components of tensors of force and moment stresses statically equivalent to them integral characteristics are introduced in micropolar theory: forces T<sub>ii</sub>, S<sub>ij</sub>, N<sub>i</sub><sub>3</sub>, N<sub>3i</sub>, moments M<sub>ii</sub>, H<sub>ij</sub>, L<sub>ii</sub>, L<sub>ij</sub>, L<sub>i</sub><sub>3</sub>, L<sub>33</sub> and hypermoments<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x83.png" xlink:type="simple"/></inline-formula>:</p><disp-formula id="scirp.58869-formula925"><label>(28)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x84.png"  xlink:type="simple"/></disp-formula><p>Displacements and rotations of points of the shell middle surface are introduced as follows:</p><disp-formula id="scirp.58869-formula926"><graphic  xlink:href="http://html.scirp.org/file/3-5300790x85.png"  xlink:type="simple"/></disp-formula><p>Satisfying boundary conditions (4) on shell surfaces <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x86.png" xlink:type="simple"/></inline-formula> taking into consideration (27), (17), following system of equations of two-dimensional problem of micropolar theory of shells with free fields of displacements and rotations will be obtained:</p><p>Equilibrium equations:</p><disp-formula id="scirp.58869-formula927"><label>(29)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x87.png"  xlink:type="simple"/></disp-formula><p>Elasticity relations:</p><disp-formula id="scirp.58869-formula928"><label>(30)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x88.png"  xlink:type="simple"/></disp-formula><p>Geometric relations:</p><disp-formula id="scirp.58869-formula929"><label>(31)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x89.png"  xlink:type="simple"/></disp-formula><p>System of equations of thin shells of classical theory will be obtained from system of Equations (29)-(31) in case of <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x90.png" xlink:type="simple"/></inline-formula> (i.e. system of equations of elastic thin shells of Timoshenko’s type [<xref ref-type="bibr" rid="scirp.58869-ref22">22</xref>] -[<xref ref-type="bibr" rid="scirp.58869-ref25">25</xref>] with some difference).</p></sec><sec id="s4"><title>4. Construction and Studying of Boundary Layers</title><p>We’ll proceed from three-dimensional Equations (1)-(3) of micropolar theory of elasticity. It is assumed that the surface of the shell edge<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x91.png" xlink:type="simple"/></inline-formula>, where stress state will be considered, is given with the help of the equation<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x91.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x92.png" xlink:type="simple"/></inline-formula>. Replacing of free variables is done on the basis of formulas:</p><disp-formula id="scirp.58869-formula930"><label>(32)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x93.png"  xlink:type="simple"/></disp-formula><p>where quantities <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x94.png" xlink:type="simple"/></inline-formula> have the same meaning as in case of internal problem.</p><p>Solution of the obtained system of boundary-value problem must satisfy homogeneous boundary conditions on surfaces <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x95.png" xlink:type="simple"/></inline-formula> of the shell:</p><disp-formula id="scirp.58869-formula931"><label>(33)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x96.png"  xlink:type="simple"/></disp-formula><p>We’ll pass to dimensionless quantities (7), (8) and introduce following notations:</p><disp-formula id="scirp.58869-formula932"><label>(34)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x97.png"  xlink:type="simple"/></disp-formula><p>As a result three-dimensional equations of micropolar theory in dimensionless form will be obtained from Equations (1)-(3) (with consideration of (7), (8)).</p><p>At level <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x98.png" xlink:type="simple"/></inline-formula> of asymptotic accuracy boundary layer divides into 4 independent systems of equations:</p><p>Force plane problem:</p><disp-formula id="scirp.58869-formula933"><label>(35)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x99.png"  xlink:type="simple"/></disp-formula><p>Force non plane problem:</p><disp-formula id="scirp.58869-formula934"><label>(36)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x100.png"  xlink:type="simple"/></disp-formula><p>Momental plane problem:</p><disp-formula id="scirp.58869-formula935"><label>(37)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x101.png"  xlink:type="simple"/></disp-formula><p>Momental non plane problem:</p><disp-formula id="scirp.58869-formula936"><label>(38)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x102.png"  xlink:type="simple"/></disp-formula><p>where<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x103.png" xlink:type="simple"/></inline-formula>.</p><p>The obtained equations of boundary layer in Cartesian coordinates <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x104.png" xlink:type="simple"/></inline-formula> with asymptotic accuracy <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x104.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x105.png" xlink:type="simple"/></inline-formula> describe SSS of plain and antiplane force and momental independent problems of micropolar theory of elasticity, taking place in semiband <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x104.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x105.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x106.png" xlink:type="simple"/></inline-formula></p><p>Requiring that solutions (35)-(38) of boundary layers have fading character when<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x107.png" xlink:type="simple"/></inline-formula>, we’ll obtain that such solutions have following important properties:</p><disp-formula id="scirp.58869-formula937"><label>(39)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x108.png"  xlink:type="simple"/></disp-formula><p>From the above introduced relations (special for micropolar theory of elasticity) following important conclusion can be done: when force and moment stresses are balanced in boundary layer, displacements and free rotations will have the same property.</p></sec><sec id="s5"><title>5. Jointing of Asymptotic Expansions of Internal Interactions Process and Boundary Layer</title><p>Considering problem of jointing of internal SSS and boundary layer, following symbolic formula must be introduced for the whole SSS of the shell:</p><disp-formula id="scirp.58869-formula938"><label>(40)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x109.png"  xlink:type="simple"/></disp-formula><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x110.png" xlink:type="simple"/></inline-formula>are called indicators of intensity of plane and antiplane boundary layers. <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x110.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x111.png" xlink:type="simple"/></inline-formula>must be chosen so that we can satisfy three-dimensional boundary conditions on shell edge<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x110.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x111.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x112.png" xlink:type="simple"/></inline-formula>.</p><p>Now the first variant of three-dimensional boundary conditions of micropolar theory of elasticity will be considered, when shell edge is loaded with forces and moments<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x113.png" xlink:type="simple"/></inline-formula>. Satisfying boundary conditions, following values will be taken for quantities r and<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x113.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x114.png" xlink:type="simple"/></inline-formula>:<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x113.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x114.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x115.png" xlink:type="simple"/></inline-formula>.</p><p>At level <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x116.png" xlink:type="simple"/></inline-formula> boundary conditions on <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x116.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x117.png" xlink:type="simple"/></inline-formula> will be as follows:</p><disp-formula id="scirp.58869-formula939"><label>(41)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x118.png"  xlink:type="simple"/></disp-formula><p>where<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x119.png" xlink:type="simple"/></inline-formula>.</p><p>Using corresponding conditions from (39) and on the basis of (41), boundary conditions for system (29)-(31) of two-dimensional equations will be obtained:</p><disp-formula id="scirp.58869-formula940"><label>(42)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x120.png"  xlink:type="simple"/></disp-formula><p>Let us study the second variant of three-dimensional boundary conditions of micropolar theory of elasticity, when displacements and rotations are given on the shell edge<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x121.png" xlink:type="simple"/></inline-formula>. Satisfying boundary conditions, following values will be taken for quantities r and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x121.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x122.png" xlink:type="simple"/></inline-formula> in (40):<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x121.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x122.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x123.png" xlink:type="simple"/></inline-formula>.</p><p>At level <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x124.png" xlink:type="simple"/></inline-formula> boundary conditions on <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x124.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x125.png" xlink:type="simple"/></inline-formula> will be as follows:</p><disp-formula id="scirp.58869-formula941"><label>(43)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x126.png"  xlink:type="simple"/></disp-formula><p>where<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x127.png" xlink:type="simple"/></inline-formula>.</p><p>With the help of conditions from (39) boundary conditions for two-dimensional model will be obtained:</p><disp-formula id="scirp.58869-formula942"><label>(44)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x128.png"  xlink:type="simple"/></disp-formula><p>Mixed three-dimensional boundary conditions are studied, when hinged support takes place.</p><p>Following values will be taken for quantities r and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x129.png" xlink:type="simple"/></inline-formula> in (40):<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x129.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x130.png" xlink:type="simple"/></inline-formula>.</p><p>At level <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x131.png" xlink:type="simple"/></inline-formula> boundary conditions on <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x131.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x132.png" xlink:type="simple"/></inline-formula> will be as follows:</p><disp-formula id="scirp.58869-formula943"><label>(45)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x133.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x134.png" xlink:type="simple"/></inline-formula> <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x134.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x135.png" xlink:type="simple"/></inline-formula> <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x134.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x135.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x136.png" xlink:type="simple"/></inline-formula> <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x134.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x135.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x136.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x137.png" xlink:type="simple"/></inline-formula> <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x134.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x135.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x136.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x137.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x138.png" xlink:type="simple"/></inline-formula> <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x134.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x135.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x136.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x137.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x138.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x139.png" xlink:type="simple"/></inline-formula></p><p>In this case, using conditions from (39), following boundary conditions of hinged-support will be obtained for two-dimensional model:</p><disp-formula id="scirp.58869-formula944"><label>(46)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x140.png"  xlink:type="simple"/></disp-formula></sec><sec id="s6"><title>6. Asymptotic Model of Micropolar Elastic Thin Shells</title><p>Thus two-dimensional theory of micropolar shells is constructed at level of initial approximation of the asymptotic method. System of equations (29)-(31) and boundary conditions (42) (or (43) or (46)) introduce the asymp- totic model of micropolar elastic thin shells with free fields of displacements and rotations.</p></sec><sec id="s7"><title>7. Applied Theory of Micropolar Elastic Thin Shells and Its Justification</title><p>Hypotheses method of construction of classical theory of elastic thin shells (i.e. Kirkhov-Love’s or refined hypotheses) has an advantage above the asymptotic method from point of view of engineering, because some simplifications were put in the base of theory, which have physical meaning and also visibility and clarity. Main problem of the construction of applied theory of micropolar elastic thin shells is the following: to formulate such hypotheses that let us reduce three-dimensional problem of micropolar theory of elasticity to adequate two- dimensional boundary-value problem. For achievement of this aim the use of qualitative aspects of asymptotic solution of three-dimensional boundary-value problem (1)-(5) of micropolar theory of elasticity is appropriate in thin domain of the shell.</p><p>In papers [<xref ref-type="bibr" rid="scirp.58869-ref12">12</xref>] -[<xref ref-type="bibr" rid="scirp.58869-ref14">14</xref>] the mentioned idea is developed: on the basis of qualitative aspects of asymptotic solution adequate hypotheses are formulated and as a result static and dynamic applied theories of micropolar elastic thin shells and plates are constructed. The accepted hypotheses are the followings:</p><p>1) During the deformation initially straight and normal to the shell middle surface fibers rotate freely in space at an angle as a whole rigid body, without changing their length and without remaining perpendicular to the deformed middle surface.</p><p>The formulated hypothesis is mathematically written as follows: tangential displacements and normal rotation are distributed in a linear law along the shell thickness:</p><disp-formula id="scirp.58869-formula945"><label>(47)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x141.png"  xlink:type="simple"/></disp-formula><p>Normal displacement and tangential rotations do not depend on coordinate<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x142.png" xlink:type="simple"/></inline-formula>, i.e.</p><disp-formula id="scirp.58869-formula946"><label>(48)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x143.png"  xlink:type="simple"/></disp-formula><p>It should be noted that from the point of view of displacements the accepted hypothesis, in essence, is Timoshenko’s kinematic hypothesis in the classical theory of elastic shells [<xref ref-type="bibr" rid="scirp.58869-ref22">22</xref>] -[<xref ref-type="bibr" rid="scirp.58869-ref25">25</xref>] . Here hypothesis (47), (48) in full we shall call Timoshenko’s generalized kinematic hypothesis in the micropolar theory of shells.</p><p>2) In the generalized Hook’s law (2) force stress <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x144.png" xlink:type="simple"/></inline-formula> can be neglected in relation to the force stresses<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x144.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x145.png" xlink:type="simple"/></inline-formula>; and analogically, moment stresses <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x144.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x145.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x146.png" xlink:type="simple"/></inline-formula> can be neglected in relation to the moment stresses<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x144.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x145.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x146.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x147.png" xlink:type="simple"/></inline-formula>.</p><p>3) During the determination of deformations, bending-torsions, force and moment stresses, first for the force stresses <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x148.png" xlink:type="simple"/></inline-formula> and moment stress <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x148.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x149.png" xlink:type="simple"/></inline-formula> we’ll take:</p><disp-formula id="scirp.58869-formula947"><label>(49)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/3-5300790x150.png"  xlink:type="simple"/></disp-formula><p>After determination of mentioned quantities, values of <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x151.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x151.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x152.png" xlink:type="simple"/></inline-formula> will be finally defined by the addition to corresponding values (49) summed up, obtained by integration of the first two and the sixth equilibrium equations from (1), for which the condition will be required, that quantities, averaged along the shells thickness, are equal to zero.</p><p>4) Quantities <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x153.png" xlink:type="simple"/></inline-formula> can be neglected in relation to 1.</p><p>Now we’ll compare main equations of applied static theory of micropolar elastic thin shells from paper [<xref ref-type="bibr" rid="scirp.58869-ref12">12</xref>] , which are constructed on the basis of above formulated hypotheses, with analogical Equations (29)-(31) of the asymptotic model. It is obvious that equilibrium Equations (29) and geometrical relations (31) are the same. Physical relations from paper [<xref ref-type="bibr" rid="scirp.58869-ref12">12</xref>] differ from physical relations (30) only with underlined terms in relations for <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x154.png" xlink:type="simple"/></inline-formula> It should be noted that underlined terms in relations for <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x154.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x155.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x154.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x155.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x156.png" xlink:type="simple"/></inline-formula> are the result of the fact, that in case of asymptotic theory in relations for <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x154.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x155.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x156.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x157.png" xlink:type="simple"/></inline-formula> quantity <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x154.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x155.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x156.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x157.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x158.png" xlink:type="simple"/></inline-formula> is not neglected in relation to<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x154.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x155.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x156.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x157.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x158.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x159.png" xlink:type="simple"/></inline-formula>. But as it is known such neglect is adopted in theories of thin shells. Analogical explanation has also underlined terms in relations for <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x154.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x155.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x156.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x157.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x158.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x159.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x160.png" xlink:type="simple"/></inline-formula> and<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x154.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x155.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x156.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x157.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x158.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x159.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x160.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x161.png" xlink:type="simple"/></inline-formula>. Thus, we can say that the general applied static theory of micropolar elastic thin shells, constructed in paper [<xref ref-type="bibr" rid="scirp.58869-ref12">12</xref>] , is asymptotically correct theory.</p><p>Concerning the dynamic theory of micropolar elastic thin shells, it should be noted that the corresponding asymptotic model is constructed in paper [<xref ref-type="bibr" rid="scirp.58869-ref26">26</xref>] , and the applied model, constructed on the basis of the above formulated hypotheses, is introduced in paper [<xref ref-type="bibr" rid="scirp.58869-ref13">13</xref>] . If we compare these two models, we’ll see that motion equations and geometrical relations (which have form (31)) are the same. Concerning physical relations we can say that the difference is underlined terms in relations (30) for<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x162.png" xlink:type="simple"/></inline-formula>.</p><p>As in case <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/3-5300790x163.png" xlink:type="simple"/></inline-formula> classical model of elastic thin shells of Timoshenko’s type will be obtained from asymptotic model (Equations (29)-(31)) and also from applied model of paper [<xref ref-type="bibr" rid="scirp.58869-ref12">12</xref>] , we can say that this classical applied refined model of thin shells is the asymptotically correct model (such conclusion can be also done in case of dynamic problem).</p><p>It should be noted that in papers [<xref ref-type="bibr" rid="scirp.58869-ref17">17</xref>] [<xref ref-type="bibr" rid="scirp.58869-ref18">18</xref>] applied theories of micropolar elastic thin plates and bars, constructed in papers [<xref ref-type="bibr" rid="scirp.58869-ref14">14</xref>] [<xref ref-type="bibr" rid="scirp.58869-ref27">27</xref>] , are justified on the basis of asymptotic method.</p></sec><sec id="s8"><title>8. Conclusions</title><p>In the present paper the question of reduction of three-dimensional boundary-value problem of micropolar and classical theories of elasticity to general applied theories of thin shells is studied. The asymptotics of singularly perturbed boundary-value problem of three-dimensional micropolar theory of elasticity is studied in thin domain of the shell. The internal iteration process and boundary-layers are constructed, jointing of these two iteration processes is studied and boundary conditions are obtained. As a result two-dimensional asymptotic model with free fields of displacements and rotations of micropolar shells is constructed. Transverse shear deformations are automatically taken into consideration in the constructed model. Particularly, classical asymptotic theory of elastic thin shells with consideration of transverse shears can be obtained from the above mentioned micropolar model.</p><p>Hypotheses are accepted for the construction of general applied theory of micropolar elastic thin shells. The hypotheses are adequate to the asymptotic behavior of the solution of three-dimensional problem. Such approach ensures the asymptotic exactness of the constructed micropolar and classical theories of thin shells with consideration of transverse shears.</p></sec><sec id="s9"><title>Cite this paper</title><p>SamvelSargsyan, (2015) Asymptotically Confirmed Hypotheses Method for the Construction of Micropolar and Classical Theories of Elastic Thin Shells. Advances in Pure Mathematics,05,629-642. doi: 10.4236/apm.2015.510057</p></sec></body><back><ref-list><title>References</title><ref id="scirp.58869-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Friedrichs, K.O. and Dressler, R.F.A. (1961) Boundary Layer Theory for Elastic Plates. Communications on Pure and Applied Mathematics, 1, 1-33. http://dx.doi.org/10.1002/cpa.3160140102</mixed-citation></ref><ref id="scirp.58869-ref2"><label>2</label><mixed-citation publication-type="other" xlink:type="simple">Green, A.E. (1962) On the Linear Theory of Thin Elastic Shells. Proceedings of the Royal Society Series A, 266, 3-25.http://dx.doi.org/10.1098/rspa.1962.0053</mixed-citation></ref><ref id="scirp.58869-ref3"><label>3</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>Vorovich</surname><given-names> I.I. </given-names></name>,<etal>et al</etal>. (<year>1966</year>)<article-title>On Some Mathematical Questions of Plate and Shell Theories</article-title><source> Proceedings of the II Union Congress of Theoretical and Applied Mechanics</source><volume> 3</volume>,<fpage> 116</fpage>-<lpage>136</lpage>.<pub-id pub-id-type="doi"></pub-id></mixed-citation></ref><ref id="scirp.58869-ref4"><label>4</label><mixed-citation publication-type="other" xlink:type="simple">Goldenvejzer, A.L. (1976) Theory of Elastic Thin Shells. Moscow. (In Russian)</mixed-citation></ref><ref id="scirp.58869-ref5"><label>5</label><mixed-citation publication-type="other" xlink:type="simple">Kaplunov, J.D., Kossovich, L.Yu. and Nolde, E.V. (1998) Dynamics of Thin Walled Elastic Bodies. Academic Press.</mixed-citation></ref><ref id="scirp.58869-ref6"><label>6</label><mixed-citation publication-type="other" xlink:type="simple">Agalovyan, L.A. (1997) The Asymptotic Theory of Anisotropic Plates and Shells. Moscow. (In Russian)</mixed-citation></ref><ref id="scirp.58869-ref7"><label>7</label><mixed-citation publication-type="other" xlink:type="simple">Rogacheva, N.N. (1994) The Theory of Piezoelectric Plates and Shells. Boca Raton, London.</mixed-citation></ref><ref id="scirp.58869-ref8"><label>8</label><mixed-citation publication-type="other" xlink:type="simple">Ustinov, Yu.A. and Shenev, M.A. (1978) On Some Directions of Development of the Asymptotic Method of Plates and Shells. Calculations of Plates and Shells, 3-27. (In Russian)</mixed-citation></ref><ref id="scirp.58869-ref9"><label>9</label><mixed-citation publication-type="other" xlink:type="simple">Sargsyan, S.H. (1992) General Two-Dimensional Theory of Magnetoelasticity of Thin Shells, Yerevan. (In Russian)</mixed-citation></ref><ref id="scirp.58869-ref10"><label>10</label><mixed-citation publication-type="other" xlink:type="simple">Altenbach, H. and Eremeyev, V.A. (2009) On the Linear Theory of Micropolar Plates. Zeitschrift fur Angewandte Mathematik und Mechanik (ZAMM), 89, 242-256. http://dx.doi.org/10.1002/zamm.200800207</mixed-citation></ref><ref id="scirp.58869-ref11"><label>11</label><mixed-citation publication-type="other" xlink:type="simple">Altenbach, J., Altenbach, H. and Eremeyev, V.A. (2009) On Generalized Cosserat-Tape Theories of Plates and Shells: A Short Review and Bibliography. Archive of Applied Mechanics, 80, 73-92.</mixed-citation></ref><ref id="scirp.58869-ref12"><label>12</label><mixed-citation publication-type="other" xlink:type="simple">Sargsyan, S.H. (2012) General Theory of Micropolar Elastic Thin Shells. Journal of Physical Mesomechanics, 15, 69-79. http://dx.doi.org/10.1134/S1029959912010079</mixed-citation></ref><ref id="scirp.58869-ref13"><label>13</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>Sargsyan</surname><given-names> S.H. </given-names></name>,<etal>et al</etal>. (<year>2011</year>)<article-title>The General Dynamic Theory of Micropolar Elastic Thin Shells</article-title><source> Reports of Physics</source><volume> 56</volume>,<fpage> 39</fpage>-<lpage>42</lpage>.<pub-id pub-id-type="doi"></pub-id></mixed-citation></ref><ref id="scirp.58869-ref14"><label>14</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>Sargsyan</surname><given-names> S.H. </given-names></name>,<etal>et al</etal>. (<year>2012</year>)<article-title>Mathematical Model of Micropolar Elastic Thin Plates and Their Strength and Stiffness Characteristics</article-title><source> Journal of Applied Mechanics and Technical Physics</source><volume> 53</volume>,<fpage> 275</fpage>-<lpage>282</lpage>.<pub-id pub-id-type="doi"></pub-id></mixed-citation></ref><ref id="scirp.58869-ref15"><label>15</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>Sargsyan</surname><given-names> S.H. </given-names></name>,<etal>et al</etal>. (<year>2008</year>)<article-title>Boundary-Value Problems of Asymmetric Theory of Elasticity for Thin Plates</article-title><source> Journal of Applied Mathematics and Mechanics</source><volume> 72</volume>,<fpage> 77</fpage>-<lpage>86</lpage>.<pub-id pub-id-type="doi"></pub-id></mixed-citation></ref><ref id="scirp.58869-ref16"><label>16</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>Sargsyan</surname><given-names> S.H. </given-names></name>,<etal>et al</etal>. (<year>2012</year>)<article-title>The Theory of Micropolar Thin Elastic Shells</article-title><source> Journal of Applied Mathematics and Mechanics</source><volume> 76</volume>,<fpage> 235</fpage>-<lpage>249</lpage>.<pub-id pub-id-type="doi"></pub-id></mixed-citation></ref><ref id="scirp.58869-ref17"><label>17</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>Sargsyan</surname><given-names> S.H. </given-names></name>,<etal>et al</etal>. (<year>2012</year>)<article-title>The Construction of Mathematical Model of Micropolar Elastic Thin Beams on the Basis of the Asymptotic Theory. News of Higer Educational Intitutes. The North Caucasus Region</article-title><source> Natural Sciences</source><volume> 5</volume>,<fpage> 31</fpage>-<lpage>37</lpage>.<pub-id pub-id-type="doi"></pub-id></mixed-citation></ref><ref id="scirp.58869-ref18"><label>18</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>Sargsyan</surname><given-names> S.H. </given-names></name>,<etal>et al</etal>. (<year>2013</year>)<article-title>The Asymptotic Method of the Construction of Mathematical Models of Micropolar Elastic Thin Plates</article-title><source> Scientific Proceedings of GSPI</source><volume> 1</volume>,<fpage> 7</fpage>-<lpage>37</lpage>.<pub-id pub-id-type="doi"></pub-id></mixed-citation></ref><ref id="scirp.58869-ref19"><label>19</label><mixed-citation publication-type="other" xlink:type="simple">Goldenveizer, A.L., Kaplunov, J.D. and Nolde, E.V. (1993) On Timoshenko-Reissner Type Theories of Plates and Shells. International Journal of Solids and Structures, 30, 675-694.</mixed-citation></ref><ref id="scirp.58869-ref20"><label>20</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>Palmov</surname><given-names> V.A. </given-names></name>,<etal>et al</etal>. (<year>1964</year>)<article-title>Basic Equations of the Theory of Asymmetric Elasticity</article-title><source> Applied Mathematics and Mechanics</source><volume> 28</volume>,<fpage> 1117</fpage>-<lpage>1120</lpage>.<pub-id pub-id-type="doi"></pub-id></mixed-citation></ref><ref id="scirp.58869-ref21"><label>21</label><mixed-citation publication-type="other" xlink:type="simple">Nowacki, W. (1986) Theory of Asymmetric Elasticity. Pergamon Press, Oxford, New York, Toronto, Sydney, Paris, Frankfurt.</mixed-citation></ref><ref id="scirp.58869-ref22"><label>22</label><mixed-citation publication-type="other" xlink:type="simple">Pelech, P.L. (1977) Stress Concentration around the Holes in Bending Transversely Isotropic Plates. Kiev. (In Russian)</mixed-citation></ref><ref id="scirp.58869-ref23"><label>23</label><mixed-citation publication-type="other" xlink:type="simple">Grigolyuk, E.I. and Kulikov, G.M. (1988) Multilayered Reinforced Shells. Calculation of Pneumatic Tires, Moscow. (In Russian)</mixed-citation></ref><ref id="scirp.58869-ref24"><label>24</label><mixed-citation publication-type="other" xlink:type="simple">Grigorenko, Y.M. and Vasilenko, A.T. (1981) Theory of Shells of Variable Stiffness. Kiev. (In Russian)</mixed-citation></ref><ref id="scirp.58869-ref25"><label>25</label><mixed-citation publication-type="other" xlink:type="simple">Percev, A.K. and Platonov, E.G. (1987) Dynamics of Plates and Shells. Leningrad. (In Russian)</mixed-citation></ref><ref id="scirp.58869-ref26"><label>26</label><mixed-citation publication-type="other" xlink:type="simple">Sargsyan, A.A. (2011) Asymptotic Analysis of Dynamic Initial Boundary-Value Problem of Asymmetric Theory of Elasticity with Free Rotations in Thin Domain of the Shell. News of NAS Armenia, Mechanics, 64, 39-50. (In Russian)</mixed-citation></ref><ref id="scirp.58869-ref27"><label>27</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>Sargsyan</surname><given-names> S.H. </given-names></name>,<etal>et al</etal>. (<year>2012</year>)<article-title>Effective Manifestations of Characteristics of Strength and Rigidy of Micropolar Elastic Thin Bars</article-title><source> Journal of Materials Science and Engineering</source><volume> 2</volume>,<fpage> 98</fpage>-<lpage>108</lpage>.<pub-id pub-id-type="doi"></pub-id></mixed-citation></ref></ref-list></back></article>