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Single-strain-gage force/stiffness buckling prediction techniques on a hat-stiffened panelPredicting the buckling characteristics of a test panel is necessary to ensure panel integrity during a test program. A single-strain-gage buckling prediction method was developed on a hat-stiffened, monolithic titanium buckling panel. The method is an adaptation of the original force/stiffness method which requires back-to-back gages. The single-gage method was developed because the test panel did not have back-to-back gages. The method was used to predict buckling loads and temperatures under various heating and loading conditions. The results correlated well with a finite element buckling analysis. The single-gage force/stiffness method was a valid real-time and post-test buckling prediction technique.
Document ID
19910009764
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hudson, Larry D.
(NASA Ames Research Center Moffett Field, CA., United States)
Thompson, Randolph C.
(PRC Systems Services Co. Edwards, CA., United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1991
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
H-1660
NAS 1.15:101733
NASA-TM-101733
Report Number: H-1660
Report Number: NAS 1.15:101733
Report Number: NASA-TM-101733
Meeting Information
Meeting: ASME Structures and Materials Conference
Location: Dallas, TX
Country: United States
Start Date: November 25, 1990
End Date: November 30, 1990
Accession Number
91N19077
Funding Number(s)
PROJECT: RTOP 505-63-31
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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