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Supersonic investigation of effects of configuration geometry on pressure-coefficient and section normal-force-coefficient distributions for a two-stage launch vehicleSupersonic study of configuration geometry effects on pressure-coefficient and section normal-force- coefficient distributions for two-stage launch vehicle
Document ID
19660024161
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
August 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3408
Report Number: NASA-TN-D-3408
Accession Number
66N33451
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUPERSONIC PRESSURE DISTRIBUTION
FORCE DISTRIBUTION
GEOMETRIC FACTOR
LAUNCH VEHICLE CONFIGURATION

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