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CENTER-LINE PRESSURE DISTRIBUTIONS ON TWO-DIMENSIONAL BODIES WITH LEADING-EDGE ANGLES GREATER THAN THAT FOR SHOCK DETACHMENT AT MACH NUMBER 6 AND ANGLES OF ATTACK UP TO 25 DEGCenter-line pressure distribution on two- dimensional bodies
Document ID
19630007425
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Ashby, G. C., Jr. (NASA Langley Research Center Hampton, VA, United States)
Goldberg, T. J. (NASA Langley Research Center Hampton, VA, United States)
Hondros, J. G. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1963
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-1793
Report Number: NASA-TN-D-1793
Accession Number
63N17301
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PRESSURE DISTRIBUTION
TWO-DIMENSIONAL BODY

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