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LARGE DEFLECTlONS AND STABlLlTY OF SHELLS OF REVOLUTlON
PROJECT STORE STRUCTURES ORlENTED RETRlEVABLE
USE OF THE COMPUTER FOR THE ELASTlC ANALYSlS
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analysis of pressure Analysis of Shells Applied Mechanics approximation ASME axial Axisymmetric behavior bodies of revolution boundary conditions buckling calculated clamped collapse pressure computer programs convergence creep law creep strain cylindrical shell deformation developed differential equations digital computer displacement elastic solution elastic-plastic example experimental finite difference finite element analysis finite element method Flight Dynamics flush nozzle geometry hypersurface information space internal pressure Kalnins large deflections limit analysis linear programming lnstitute lnternal Pressure Load deflection curves lower bound Marcal Matrix maximum Mech Mises nondimensional Nonlinear programming nonsymmetric loads numerical integration numerical procedure obtained P-8 curve perfectly plastic plane plate pressure vessel purpose program radius Rashid Report Research Shells of Revolution shown in Figure solved spherical cap steady creep strain hardening strain rates Stress Analysis stress strain relations symmetric techniques thick thin shell three dimensional problems time-shared tion transient creep Wempner yield criterion