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aluminum average stress bending bottom face calculated composite materials compressive and tensile Compressive stress concentrated load creep cross-sectional area CY D4 D—IN DC—IN deflection and stresses deflection due derived in chapter Differentiating Distance between neutral dM/dx due to shear dVdx2 dy/dx e-CY El—PSI E2—PSI elastic modulus Elongation equal equation XVII equation XXXV equations derived face2 facei flat faces foam foam-filled panel foam-filled sandwich foam-filled structures FORMAT Fortran G—PSI GbD2 GCLD Integrating maximum moments of inertia neutral axis numbers panel under uniform panel with thin REAL 101 REAL respective faces rigid faces sandwich beam shear modulus shear stress shown in Figure simplified equations simply supported single solution Stress in Faces supported single span sustained load Table TECHNOMIC tensile forces tensile stress thermal expansion thermal warp thickness THWRP top face trial value uniform load UNILD value of G width XXXVI