Postwrinkling behavior of a conical shell of revolution subjected to bending loads
Postwrinkling nonlinear behavior of conical shell of revolution subjected to bending loads
Conroy, D. C.↗
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Numerical analysis of finite axisymmetric deformations of incompressible elastic solids of revolution
Finite element method applicaions to finite axisymmetric deformations of incompressible elastic solids of revolution
Key, J. E.↗
Nonlinear dynamic analysis of shells of revolution by matrix displacement method
Nonlinear dynamic analysis of shells of revolution under symmetric and asymmetric loads, obtaining solutions for shallow cap buckling
Haisler, W. E.↗
Numerical methods for mixed boundary value problems of shells of revolution
Numerical methods for mixed boundary value problem of axisymmetric shells of revolution, using truncated series expansion and finite difference expressions
Kalnins, A.↗
A program for the nonlinear static and dynamic analysis of arbitrarily loaded shells of revolution
Computer program for geometrical nonlinear static and dynamic structural analysis of arbitrarily loaded shells of revolution
Ball, R. E.↗
Stress, buckling, and vibration analysis of shells of revolution
Stress, buckling and vibration analysis of shells of revolution by numerical integration and finite difference methods, summarizing computer programs
Anderson, M. S.↗
Computer program for predicting creep behavior of bodies of revolution
Computer program, CRAB, uses finite-element method to calculate creep behavior and predict steady-state stresses in an arbitrary body of revolution subjected to a time-dependent axisymmetric load. Creep strains follow a time hardening law and a Prandtl-Reuss stress-strain relationship.
Adams, R.↗
Vibration characteristics of ring-stiffened orthotropic shells of revolution
Computer program solves vibration modes and frequencies of thin shells of revolution having general meridional curvature and orthotropic elastic properties in order to evaluate the dynamic behavior of structures with thin shelled components.
Adelman, H. M.↗
Numerical methods of integration applied in the nonlinear dynamic analysis of shells of revolution
Evaluating methods of numerically integrating equations of motion for nonlinear dynamic analyses of shells of revolution by matrix displacement method
Stricklin, J. A.↗
Boundary-layer transition study of several pointed bodies of revolution at supersonic speeds
Boundary layer transition studies of several pointed bodies of revolution at supersonic speeds
Campbell, J. F.↗
User's manual for a digital computer program for computing the vibration characteristics of ring-stiffened orthotropic shells of revolution
Digital computer program for computing vibration characteristics of ring-stiffened orthotropic shells of revolution - users manual
Adelman, H. M.↗
Computer program for finite-difference solutions of shells of revolution under asymmetric dynamic loading
Computer program for finite difference solutions of shells of revolution under asymmetric dynamic loading
Robinson, M. P.↗
Minimum-mass isotropic shells of revolution subjected to uniform pressure and axial load
Minimum mass isotropic shells of revolution under uniform pressure and axial loads
Stroud, W. J.↗
SAMMSOR 2 - A finite element program to determine Stiffness And Mass Matrices of Shells Of Revolution
Finite element program for determining stiffness and mass matrices of shells of revolution - users manual
Haisler, W. E.↗
Computer program for static and dynamic axisymmetric nonlinear response of symmetrically loaded orthotropic shells of revolution
Computer program for determining static and dynamic response of symmetrically loaded elastic orthotropic shells of revolution
Stephens, W. B.↗
DYNASOR 2 - A finite element program for the dynamic nonlinear analysis of shells of revolution
DYNASOR-2 finite element program for dynamic nonlinear analysis of shells of revolution
Haisler, W. E.↗
Calculation of temperature distributions in thin shells of revolution by the finite element method
Computer program using finite element method for computing temperature distributions in thin shells of revolution
Adelman, H. M.↗
A wind-tunnel investigation of sonic-boom pressure distributions of bodies of revolution at Mach 2.96, 3.83, and 4.63
Measurements of sonic boom pressure distribution of bodies of revolution at Mach 2.96, 3.83, and 4.63 in Unitary Plan wind tunnel
Dollyhigh, S. M.↗