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CF6 jet engine performance improvement program. Short core exhaust nozzle performance improvement conceptThe short core exhaust nozzle was evaluated in CF6-50 engine ground tests including performance, acoustic, and endurance tests. The test results verified the performance predictions from scale model tests. The short core exhaust nozzle provides an internal cruise sfc reduction of 0.9 percent without an increase in engine noise. The nozzle hardware successfully completed 1000 flight cycles of endurance testing without any signs of distress.
Document ID
19790025035
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Fasching, W. A.
(General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 3, 2013
Publication Date
September 1, 1979
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-159564
Report Number: NASA-CR-159564
Accession Number
79N33206
Funding Number(s)
CONTRACT_GRANT: NAS3-20629
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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