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Flow field survey and decelerator drag characteristics in the wake of a model of the X-15 airplane at Mach 2.30 and 4.65Flow field survey and decelerator drag characteristics in wake of model X-15 airplane at Mach 2.30 and 4.65
Document ID
19660007274
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Campbell, J. F. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3285
Report Number: NASA-TN-D-3285
Accession Number
66N16563
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WIND TUNNEL
FLOW FIELD
DECELERATION
X-15 AIRCRAFT

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