Research Catalog

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

Title
Improved assumed-stress hybrid shell element with drilling degrees of freedom for linear stress, buckling and free vibration analyses [microform] / Govid Rengaranjan, Mohammad A. Aminpour, Norman F. Knight.
Author
Rengaranjan, Govid.
Publication
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]

Details

Additional Authors
  • Aminpour, Mohammad A.
  • Knight, Norman F.
  • United States. National Aeronautics and Space Administration.
Description
1 v.
Series Statement
NASA contractor report ; NASA CR-192816
Alternative Title
Improved assumed stress hybrid shell element with drilling degrees of freedom for linear sress, bucking and free vibration analyses
Subject
  • Buckling
  • Degrees of freedom
  • Dynamic structural analysis
  • Finite element method
  • Free vibration
  • Shells (Structural forms)
  • Stress analysis
Note
  • Distributed to depository libraries in microfiche.
  • Shipping list no.: 95-0052-M.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.26:192816
OCLC
marcive32155403
Author
Rengaranjan, Govid.
Title
Improved assumed-stress hybrid shell element with drilling degrees of freedom for linear stress, buckling and free vibration analyses [microform] / Govid Rengaranjan, Mohammad A. Aminpour, Norman F. Knight.
Imprint
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1992]
Series
NASA contractor report ; NASA CR-192816
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 1 microfiche.
Added Author
Aminpour, Mohammad A.
Knight, Norman F.
United States. National Aeronautics and Space Administration.
Gpo Item No.
0830-H-14 (MF)
Sudoc No.
NAS 1.26:192816
Research Call Number
READEX Microfiche NAS 1.26:192816
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