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A. J. S. Pippard angle assumed axial axis beam bow girder braced bulkhead calculated component compression connected considered cos2 cosec cross-sectional area curved member deflection determined direction of W2 due to bending equilibrium equivalent evaluated example external load system fixed flexural rigidity force H framework fuselage gives Hence Hooke's law hoop stress integrals just-stiff frame length longeron M0 and H material modulus of elasticity movement necessary number of bars obtained perpendicular pinned plane frame point of application polygon radius reacting forces redundant members resultant actions rigidity ring rth side shear stress shearing force shown in Fig Simpson's rule space frame static static equilibrium statically indeterminate stiff joints straight members strain energy due Strength of Materials STRESS ANALYSIS stress diagram structure struts supports Suppose symmetry tangential tangential component temperature torque Torsional total strain energy truss values of M0 vertical wall