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NASA NTRS · 19910009764

Single-strain-gage force/stiffness buckling prediction techniques on a hat-stiffened panel

Abstract

Predicting 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.

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BibTeXRIS

Hudson, Larry D., Thompson, Randolph C.. 1991-02-01. Single-strain-gage force/stiffness buckling prediction techniques on a hat-stiffened panel. https://ntrs.nasa.gov/citations/19910009764

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