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
01.05.1994
Sonstige
Keine Angabe
Englisch
Verifying Stiffness Parameters of Filament-Wound Cylinders
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