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An empirical method for determining static distributed aerodynamic loads on axisymmetric multistage launch vehiclesEmpirical method for determining static distributed aerodynamic loads on axisymmetric multistage launch vehicles
Document ID
19660010176
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Muraca, R. J. (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-3283
Accession Number
66N19465
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AERODYNAMIC LOAD
MULTISTAGE ROCKET VEHICLE
STATIC LOADING
AXISYMMETRIC BODY
LOAD DISTRIBUTION

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