Improved assumed-stress hybrid shell element with drilling degrees of freedom for linear stress, buckling and free vibration analyses

Improved assumed-stress hybrid shell element with drilling degrees of freedom for linear stress, buckling and free vibration analyses

Saved in:
Bibliographic Details
Main Author: Rengarajan, Govind
Corporate Author: United States National Aeronautics and Space Administration
Other Authors: Aminpour, Mohammad A (Mohammad Ali), Knight, Norman F
Format: Government Document Book
Language:English
Published: [Washington, DC : Springfield, Va. : National Aeronautics and Space Administration ; National Technical Information Service, distributor, 1992]
Series:NASA contractor report NASA CR-192816
Subjects:
Buckling
Degrees of freedom
Dynamic structural analysis
Finite element method
Free vibration
Shells (Structural forms)
Stress analysis
Tags: Add Tag
No Tags, Be the first to tag this record!
Description
Item Description:Distributed to depository libraries in microfiche
Shipping list no.: 95-0052-M
Physical Description:1 v

Similar Items