Conical shell deflection and acceleration response program /darc/
IBM 7094 computer program for calculation of truncated conical shell deflection and acceleration response
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IBM 7094 computer program for calculation of truncated conical shell deflection and acceleration response
Structural stability of shells - random pressure excitation and statistical dependence of normal mode response
Conical shells with linear thickness variation subjected to lateral normal loads
Membrane analysis of very thin pressurized spheroid shells composed of flat gores - application to Echo II satellite
Structural efficiency of orthotropic materials for cylindrical shells under axial load, including examination of fibrous composites characteristics
Finite element approach to analysis of axisymmetric thin elastic shells, employing matrix method
Shell motion equations derived in terms of reference state from three-dimensional theory based on Cauchy motion laws for undeformed bodies
Fibrous composite shell structural efficiency as function of constituent properties
Transverse stiffness of pressurized thin elastic shells of revolution under external load determined as function of internal pressure
Tension shell configurations developed for low structural density entry capsules for exploration of Mars and other planets
Resonant frequencies and mode shapes for transverse vibration of truncated conical shells obtained by considering effect of bending, membrane rigidity and inertia terms due to transverse motion
Pressurized cylindrical shell under axial load, considering types of buckling and effects of asymmetric and axisymmetric imperfections
Numerical techniques for digital computer solution of algebraic simultaneous linear equations from finite difference approximation of partial differential equations of thin elastic shells
Fortran IV computer program for evaluation of natural frequencies and unstable values of thrust frequency for free-free circular cylindrical shell subjected to end thrust
Thermal buckling characteristics of flanged thin shell leading edges - aerodynamic heating
Axisymmetric deformation effects on cylindrical shell buckling under axial compression
Orthotropic cylindrical shell buckling under axial compression - structural dynamics
Matrix algebra solution, using coordinate systems transformations, to boundary value problem for structures composed of shell elements