Page 221 - Analysis and Design of Energy Geostructures
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194   Analysis and Design of Energy Geostructures


                d. The thermally induced strain of materials subjected to thermal loads is

                    governed by the material linear thermal expansion coefficient α με= C

                    and the applied temperature variation ΔT ½ CŠ.

                 e. The unit measure of the linear thermal expansion coefficient is:

                     i. C
                    ii. m/ C

                    iii. C/m

                    iv. 1/ C

                 f. For an infinitesimal element that is free to deform and solely subjected to
                    a thermal load, the induced strain is spherical (volumetric) and can be
                    expressed in tensor form as
                                              2                             3
                                                2 αΔT        0         0
                                   ε ij 5 ε th  5  0      2 αΔT        0
                                         ij;f  4                            5
                                                   0         0      2 αΔT


                    where α με= C is the material linear thermal expansion coefficient and

                    ΔT ½ CŠ is the applied temperature variation.
                 g. The compatibility equations imply that the deformation of a continuum
                    material occurs without creating any gaps or overlaps.
                 h. The stress tensor describes the stress state of any infinitesimal three-
                    dimensional element of a considered material subjected to loading. It is a
                    symmetric tensor characterised by nine stress components that in rectan-
                    gular Cartesian coordinates reads:

                                        2                3   2              3
                                          σ xx  σ xy  σ xz     σ x  τ xy  τ xz
                                   σ ij 5  4  σ yx  σ yy  σ yz  5  5 τ yx  σ y  τ yz  5
                                                             4
                                          σ zx  σ zy  σ zz    τ zx  τ zy  σ z
                       The diagonal components σ kk [Pa] of the stress tensor expressed in
                    relation act normal to the coordinate planes and are called normal stres-
                    ses. The off-diagonal components σ kl [Pa] act tangential to the coordi-
                    nate planes and are called shear stresses.
                       The stress tensor is symmetric and this property can be proven con-
                    sidering the principle of balance of angular momentum. As a result, the
                    complementary components of the shear stress are equal:


                                                    σ xy 5 σ yx
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