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Investigation of methods for predicting flow in the shock layer over bodies at small angles of attackLinearized characteristics method, and equivalent body method for predicting flow field about axisymmetric body at small angle of attack
Document ID
19670014525
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Gallo, W. F. (NASA Ames Research Center Moffett Field, CA, United States)
Rakich, J. V. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1967
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TN-D-3946
Report Number: NASA-TN-D-3946
Accession Number
67N23854
Funding Number(s)
CONTRACT_GRANT: 126-15-03-01-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AXISYMMETRIC BODY
PREDICTION THEORY
FLOW FIELD

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