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Jet effects at supersonic speeds on base and afterbody pressures of a missile model having single and multiple jetsPressure distribution on base and afterbody of missile configuration with and without jet flow using single and multiple nozzles
Document ID
19640000611
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Charczenko, N. (NASA Langley Research Center Hampton, VA, United States)
Hayes, C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1963
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-2046
Report Number: NASA-TN-D-2046
Accession Number
64N10520
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
MISSILE CONFIGURATION
PRESSURE DISTRIBUTION

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