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Stagnation and static pressures on a nose-mounted 15 deg conical probe with various forebody configurationsPressure distribution data at subsonic and transonic speeds for calibrating hypersonic conical pressure probe for X-15 aircraft
Document ID
19660023728
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Coates, E. M., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3526
Report Number: NASA-TN-D-3526
Accession Number
66N33018
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PRESSURE DISTRIBUTION
TRANSONIC SPEED
X-15 AIRCRAFT

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