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Effects of Simulated Rocket-jet Exhaust on Stability and Control of a Research-type Airplane Configuration at a Mach Number of 6.86Simulated rocket jet exhaust effect on stability and control of research aircraft configuration
Document ID
19650018534
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Fetterman, D. E., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1959
Subject Category
Biosciences
Report/Patent Number
NASA-TM-X-127
Accession Number
65N28135
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
RESEARCH AIRCRAFT
JET EXHAUST
AIRCRAFT CONFIGURATION
STABILITY TEST

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