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LOCAL PRESSURE DISTRIBUTION ON A BLUNT DELTA WING FOR ANGLES OF ATTACK UP TO 35 DEG AT MACH NUMBERS OF 3.4 AND 4.7Local pressure distribution on a blunt delta wing
Document ID
19630000926
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Kussoy, M. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1962
Subject Category
Auxiliary Systems
Report/Patent Number
NASA-TN-D-1554
Report Number: NASA-TN-D-1554
Accession Number
63N10800
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PRESSURE DISTRIBUTION
TUNING FORK GYROSCOPE
DELTA WING

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