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Energy efficient engine component development and integration programThe design of an energy efficient commercial turbofan engine is examined with emphasis on lower fuel consumption and operating costs. Propulsion system performance, emission standards, and noise reduction are also investigated. A detailed design analysis of the engine/aircraft configuration, engine components, and core engine is presented along with an evaluation of the technology and testing involved.
Document ID
19840024319
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 4, 2013
Publication Date
December 19, 1980
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
PWA-5594-142
NAS 1.26:173884
SASR-5
NASA-CR-173884
Report Number: PWA-5594-142
Report Number: NAS 1.26:173884
Report Number: SASR-5
Report Number: NASA-CR-173884
Accession Number
84N32389
Funding Number(s)
CONTRACT_GRANT: NAS3-20646
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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