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Aerodynamic characteristics of wing-body and lifting-body configurations of hypersonic cruise aircraft at Mach 2.30 to 4.63Wind tunnel investigation of aerodynamic characteristics of wing-body and lifting body configurations for hypersonic cruise aircraft at hypersonic speeds
Document ID
19710019385
Document Type
Technical Memorandum (TM)
Authors
Jernell, L. S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1971
Subject Category
Aircraft
Report/Patent Number
L-7229
NASA-TM-X-2287
Funding Number(s)
CONTRACT_GRANT: 722-01-10-07
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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