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Integral approach to the yawed blunt body problem.Inviscid gas flow over nose region of supersonic yawed axisymmetric blunt body treated by integral relations in body oriented coordinate system
Document ID
19650031862
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Waldman, G. D.
Date Acquired
August 2, 2013
Publication Date
January 1, 1965
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 65-28
Report Number: AIAA PAPER 65-28
Accession Number
65A14566
Funding Number(s)
CONTRACT_GRANT: NAS9-858
CONTRACT_GRANT: NAS9-2494
Distribution Limits
Public
Copyright
Other
Keywords
SUPERSONIC FLOW
INTEGRAL FUNCTION
INVISCID FLOW
BLUNT BODY
AXISYMMETRIC BODY

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