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Effects of wing elevation, incidence, and camber on the aerodynamic characteristics of a representative hypersonic cruise configuration at Mach numbers from 0.65 to 10.70Wing elevation, incidence, and chamber effects on aerodynamic characteristics of representative hypersonic cruise configuration at Mach numbers from 0.65 to 10.70
Document ID
19700033421
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Axelson, J. A. (NASA Ames Research Center Moffett Field, CA, United States)
Nelms, W. P., Jr. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1970
Subject Category
Aerodynamics
Report/Patent Number
A-3701
NASA-TN-D-6049
Report Number: A-3701
Report Number: NASA-TN-D-6049
Accession Number
70N42737
Funding Number(s)
CONTRACT_GRANT: 722-01-10-02-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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