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Pressure Distribution of a 0.0667-Scale Model of the X-15 Airplane for an Angle-Of-Attack Range of 0 deg To 28 deg at Mach Numbers of 2.30, 2.88, and 4.65Pressure distribution on x-15 aircraft model
Document ID
19630002770
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Burbank, P. B. (NASA Langley Research Center Hampton, VA, United States)
Hodge, B. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1960
Subject Category
Biosciences
Report/Patent Number
NASA-TM-X-275
Report Number: NASA-TM-X-275
Accession Number
63N12646
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PRESSURE DISTRIBUTION
X-15A AIRCRAFT
AIRCRAFT MODEL
AERODYNAMICS
YAW
WIND TUNNEL

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