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CHAPTER PAgE 1 STRUCTURAL ANALYSIS METHODS
FORCES AND MOMENTS
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actual airplane aluminum alloy analysis analytical angle applied assumed assumption axial force axial loading axial stress bending stresses Calculate centroid Chapt combined components compression stress computed conventions cross section cross-sectional area curve deflection determined diagonal diameter direction distance effect elastic equal equations of equilibrium example failure Figure force transmission forces acting formula frame hence indicated in Fig inertia joint line of action loading condition material measured method modulus Mohr's circle moments of inertia multiplied neutral axis Note obtained parallel plane plastic bending Poisson's ratio principal axes Problem pure shear radius of curvature reactions represents resist resultant force rivet rotation shear center shear flow shear force shear load shear stress sheet shell shown in Fig shows simple slope static statically indeterminate steel strain stress distribution stress-strain diagram structure summation thickness tion torsion transmitted transverse force truss tube unit length usually vector vertical yield stress zero