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An investigation of two variations of the gas generator method to calculate the thrust of the afterburning turbofan engines installed in an F-111A airplaneTwo variations of gas generator method to calculate thrust of afterburning turbofan engines installed in F-111A aircraft
Document ID
19710013138
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Burcham, F. W., Jr. (NASA Flight Research Center Edwards, CA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1971
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TN-D-6297
H-643
Report Number: NASA-TN-D-6297
Report Number: H-643
Accession Number
71N22614
Funding Number(s)
CONTRACT_GRANT: 126-15-02-02-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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