NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Titanium Honeycomb Panel TestingThermal-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.
Document ID
19970002982
Acquisition Source
Armstrong Flight Research Center
Document Type
Conference Paper
Authors
Richards, W. Lance (NASA Dryden Flight Research Center Edwards,CA United States)
Thompson, Randolph C. (PRC Systems Services Co. Edwards, CA United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1996
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-4768
NAS 1.15:4768
H-2133
Report Number: NASA-TM-4768
Report Number: NAS 1.15:4768
Report Number: H-2133
Meeting Information
Meeting: Structural Testing Technology at High Temperature Conference
Location: Dayton, OH
Country: United States
Start Date: November 4, 1991
End Date: November 6, 1991
Accession Number
97N11761
Funding Number(s)
PROJECT: RTOP 505-63-40
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available