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Transonic pressure distributions over protuberances and adjacent areas in proximity to the nose of a launch vehiclePressure distribution studies in wind tunnel at Mach numbers 0.4 to 1.2 for protuberances and adjacent areas on nose of launch vehicle
Document ID
19660009744
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Blackwell, J. A., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3216
Report Number: NASA-TN-D-3216
Accession Number
66N19033
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
NOSE CONE
WIND TUNNEL
LAUNCH VEHICLE
PRESSURE DISTRIBUTION

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