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An experimental and theoretical investigation of a symmetrical and a cambered delta wing configuration at Mach numbers from 2.0 to 10.7Experimental and theoretical study of symmetrical and cambered delta wing configuration between Mach 2.0 and 10.7
Document ID
19690019891
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Carmichael, R. L. (NASA Ames Research Center Moffett Field, CA, United States)
Castellano, C. R. (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
June 1, 1969
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-5272
Accession Number
69N29269
Funding Number(s)
CONTRACT_GRANT: 126-13-03-01-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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