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Effects of rocket jet on stability and control at high Mach numbersPaper presents the results of an investigation to determine the jet-interference effects which may occur at high jet static-pressure ratios and high Mach numbers. Tests were made in the Langley 11-inch hypersonic tunnel at a Mach number of 6.86.
Document ID
19930092383
Acquisition Source
Legacy CDMS
Document Type
None
Authors
Fetterman, David E , Jr
Date Acquired
August 15, 2013
Publication Date
July 30, 1958
Accession Number
93R21673
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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