Improved assumed-stress hybrid shell element with drilling degrees of freedom for linear stress, buckling and free vibration analyses
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Author
Contributions
- Aminpour, Mohammad A. - Contributor
- Knight, Norman F. - Contributor
- United States. National Aeronautics and Space Administration. - Contributor
Publication
1992 - National Aeronautics and Space Administration, [Washington, DC, District of Columbia
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Physical Format
Microform
Identifiers
- Open LibraryOL18075912M
Alternate Titles
- Improved assumed stress hybrid shell element with drilling degrees of freedom for linear sress, bucking and free vibration analyses.
Subjects
Series Statement
- NASA contractor report -- NASA CR-192816.
Other Editions
- Improved assumed-stress hybrid shell element with drilling degrees of freedom for linear stress, buckling and free vibration analyses
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