Improved assumed-stress hybrid shell element with drilling degrees of freedom for linear stress, buckling and free vibration analyses
By: Govid Rengaranjan, Mohammad A. Aminpour, Norman F. Knight.
Contributors: Aminpour, Mohammad A.; Knight, Norman F.; United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- NASA CR-192816.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1992
Place of publication: [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Buckling.; Degrees of freedom.; Dynamic structural analysis.; Finite element method.; Free vibration.; Shells (Structural forms); Stress analysis.
Other titles: Improved assumed stress hybrid shell element with drilling degrees of freedom for linear sress, bucking and free vibration analyses.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0052-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 1 microfiche.