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Chapter 2.  Ftindanlentn1.v of mechanics of solids   49
            integrated  if  strains satisfy six compatibility  equations, Eqs. (2.35). We can write
            these equations in terms of stresses using constitutive equations, Eq. (2.48). Thus,
            the stress formulation of the problem is reduced to a set of nine equations consisting
            of three equilibrium equations and six compatibility equations in terms of  stresses.
            At  first glance  it  looks like  this set  is  not  consistent  because  it  includes  only  six
            unknown  stresses.  However,  this is  not  the  case because  of  special properties  of
            compatibility equations. As  was noted  in  Section 2.7, these equations provide the
            existence of Euclidean space inside the deformed body. But this space automatically
            exists if  strains can be expressed in  terms of three continuous displacements as in
            Eqs. (2.22).  Indeed,  substituting  strains,  Eqs. (2.22), into compatibility equations,
            Eqs. (2.35),  we  can  readily  see  that  they  are  identically  satisfied  for  any
            three  functions  u,,  uV, and  u,.  This  means  that  the  solution  of  six  Eqs. (2.35)
            including six strains is not unique. The uniqueness is ensured by three equilibrium
           equations.



            2.11.  Variational principles

              Equations  of  Solid  Mechanics considered  in  the previous  sections can  be  also
           derived  from variational  principles  that establish the energy criteria  according to
            which the actual state of the body  under loading can be singled out of a system of
            admissible states (see Section 2.8).
             Consider a linear elastic solid and introduce two mutually independent fields of
           variables:  statically  admissible stress field ut,01..  u;,T:),  T:,   t:_  and kinematically
            admissible field characterized by displacements u:,  u:I, uy  and corresponding strains
                  /I
            L, ,E,,  E,,  y,, ,y:=,  yyc.  To construct the energy criteria allowing us to distinguish the
            I/
                     I/
               I/
            actual variables from admissible ones, consider the following integral similar to the
            energy integral in  Eqs. (2.51) and (2.52)
                                                                             (2.58)


            Here,  in  accordance  with  the  definition  of  a  kinematically  admissible  field  (see
            Section 2.8).


                                                                             (2.59)


            Substituting Eqs. (2.59) into Eq. (2.58) and  using  the  following evident  relation-
            ships between the derivatives
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