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Structures performance, benefit, cost-studyNew technology concepts and structural analysis development needs which could lead to improved life cycle cost for future high-bypass turbofans were studied. The NASA-GE energy efficient engine technology is used as a base to assess the concept benefits. Recommended programs are identified for attaining these generic structural and other beneficial technologies.
Document ID
19810022652
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Woike, O. G. (General Electric Co. Cincinnati, OH, United States)
Salemme, C. (General Electric Co. Cincinnati, OH, United States)
Stearns, E. (General Electric Co. Cincinnati, OH, United States)
Oritz, P. (General Electric Co. Cincinnati, OH, United States)
Roberts, M. L. (General Electric Co. Cincinnati, OH, United States)
Baughman, J. L. (General Electric Co. Cincinnati, OH, United States)
Johnston, R. P. (General Electric Co. Cincinnati, OH, United States)
Demel, H. F. (General Electric Co. Cincinnati, OH, United States)
Stabrylla, R. G. (General Electric Co. Cincinnati, OH, United States)
Coffinberry, G. A. (General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1981
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-165456
R81AEG393
Report Number: NASA-CR-165456
Report Number: R81AEG393
Accession Number
81N31194
Funding Number(s)
CONTRACT_GRANT: NAS3-22049
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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