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Blunt slipstream calculation using the method of integral relationsCompressible, inviscid secondary injection and primary flows calculated using integral relation method for blunt bodies - application to thrust vector control
Document ID
19660016279
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Chenoweth, D. R. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
August 3, 2013
Publication Date
April 1, 1965
Subject Category
Fluid Mechanics
Report/Patent Number
HREC-6-74-65-1
LMSC/HREC-A710967
Report Number: HREC-6-74-65-1
Report Number: LMSC/HREC-A710967
Accession Number
66N25568
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
BLUNT BODY
INVISCID FLOW
THRUST VECTOR CONTROL /TVC/
COMPRESSIBLE FLOW
SECONDARY INJECTION

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