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Some Advances in Techniques for Free-flight Testing in Hypersonic Wind TunnelsFree-flight techniques for hypersonic wind tunnel - measurement of local pressure and heat transfer and aerodynamic characteristics of model under steady-state ablation conditions
Document ID
19650019778
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Levy, L. L., Jr. (NASA Ames Research Center Moffett Field, CA, United States)
Mc Devitt, J. B. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1964
Subject Category
Facilities, Research, And Support
Report/Patent Number
NASA-TM-X-54707
Accession Number
65N29379
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HYPERSONIC WIND TUNNEL
AERODYNAMIC HEAT TRANSFER
PRESSURE
FREE FLIGHT TEST APPARATUS
ABLATION

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