NASA NTRS · 19970002982
Titanium Honeycomb Panel Testing
Abstract
Thermal-mechanical tests were performed on a titanium honeycomb sandwich panel to experimentally validate the hypersonic wing panel concept and compare test data with analysis. Details of the test article, test fixture development, instrumentation, and test results are presented. After extensive testing to 900 deg. F, non-destructive evaluation of the panel has not detected any significant structural degradation caused by the applied thermal-mechanical loads.
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Richards, W. Lance, Thompson, Randolph C.. 1996-10-01. Titanium Honeycomb Panel Testing. https://ntrs.nasa.gov/citations/19970002982
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