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Compressive buckling analysis of hat-stiffened panelBuckling analysis was performed on a hat-stiffened panel subjected to uniaxial compression. Both local buckling and global buckling were analyzed. It was found that the global buckling load was several times higher than the buckling load. The predicted local buckling loads compared favorably with both experimental data and finite-element analysis.
Document ID
19910018278
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Ko, William L. (NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Jackson, Raymond H. (NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1991
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-4310
H-1724
NAS 1.15:4310
Report Number: NASA-TM-4310
Report Number: H-1724
Report Number: NAS 1.15:4310
Accession Number
91N27592
Funding Number(s)
PROJECT: RTOP 505-63-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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