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Comparison of measured and calculated temperatures for a Mach 8 hypersonic wing test structureStructural temperatures were measured on a hypersonic wing test structure during a heating test that simulated a Mach 8 thermal environment. Measured data are compared to design calculations and temperature predictions obtained from a finite-difference thermal analysis.
Document ID
19860013092
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Quinn, R. D. (NASA Ames Research Center Moffett Field, CA, United States)
Fields, R. A. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1986
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NAS 1.15:85918
A-85137
NASA-TM-85918
H-1271
Accession Number
86N22563
Funding Number(s)
PROJECT: RTOP 506-53-51
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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