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Pressures and heat transfer on a 75 degree swept delta wing with trailing-edge flap at Mach 6 and angles of attack to 90 degreesPressure and heat transfer on swept delta wing with trailing-edge flap
Document ID
19690026477
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Keyes, J. W. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1969
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-5418
Report Number: NASA-TN-D-5418
Accession Number
69N35855
Funding Number(s)
CONTRACT_GRANT: 126-13-10-19-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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