Predicted engineering stiffness parameters of filament-wound composite-material cylinders verified with respect to experimental data, by use of equations developed straightforwardly from applicable formulation of Hooke's law. Equations derived in engineering study of filament-wound rocket-motor cases, also applicable to other cylindrical pressure vessels made of orthotropic materials.
Verifying Stiffness Parameters Of Filament-Wound Cylinders
NASA Tech Briefs ; 18 , 5
1994-05-01
Miscellaneous
No indication
English
Verifying Stiffness Parameters of Filament-Wound Cylinders
Online Contents | 1994
Damping of filament wound composite cylinders
AIAA | 1996
|Damping of Filament Wound Composite Cylinders
British Library Conference Proceedings | 1996
|Stiffness properties of filament wound structures
AIAA | 1966
|