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Exploratory investigation of flow field resulting from forward-facing nozzles exhausting near a large cylindrical body at free-stream Mach numbers of 3.0 and 6.0Flow field from forward facing nozzles exhausting near large cylindrical body at free-stream Mach numbers of 3.0 and 6.0
Document ID
19690011638
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Martin, J. A. (NASA Langley Research Center Hampton, VA, United States)
Mc Ghee, R. J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1969
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-5030
Accession Number
69N21000
Funding Number(s)
CONTRACT_GRANT: 126-13-03-39-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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