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Design of a V/STOL propulsion system for a large-scale fighter modelModifications were made to the existing Large-Scale STOL fighter model to simulate a V/STOL configuration. Modifications include the substitutions of two dimensional lift/cruise exhaust nozzles in the nacelles, and the addition of a third J97 engine in the fuselage to suppy a remote exhaust nozzle simulating a Remote Augmented Lift System. A preliminary design of the inlet and exhaust ducting for the third engine was developed and a detailed design was completed of the hot exhaust ducting and remote nozzle.
Document ID
19810016539
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Willis, W. S.
(General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1981
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-166162
R81AEG257
Report Number: NASA-CR-166162
Report Number: R81AEG257
Accession Number
81N25074
Funding Number(s)
CONTRACT_GRANT: NAS2-10556
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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