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Experimental investigation of secondary jets from two-dimensional nozzles with various exit Mach numbers for hypersonic control applicationSecondary jets from two-dimensional nozzles with various exit Mach numbers for hypersonic control application
Document ID
19670006335
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Alston, D. W. (NASA Langley Research Center Hampton, VA, United States)
Barber, J. B. (NASA Langley Research Center Hampton, VA, United States)
Romeo, D. J. (NASA Langley Research Center Hampton, VA, United States)
Sterrett, J. R. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1967
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3795
Report Number: NASA-TN-D-3795
Accession Number
67N15664
Funding Number(s)
CONTRACT_GRANT: 129-01-09-15-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TWO-DIMENSIONAL JET
AERODYNAMICS
HYPERSONIC VEHICLE
EXHAUST NOZZLE

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