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Optimization of engines for commercial air transports designed for cruise speeds ranging from Mach 0.90 to Mach 0.98Cost estimations, noise constraints, and supercritical wing compatibility in optimization of turbofan engines for Mach 0.90 to Mach 0.98 commercial air transports
Document ID
19710023770
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kraft, G. A. (NASA Lewis Research Center Cleveland, OH, United States)
Whitlow, J. B., Jr. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1971
Subject Category
Propulsion Systems
Report/Patent Number
E-6515
NASA-TM-X-67906
Report Number: E-6515
Report Number: NASA-TM-X-67906
Accession Number
71N33246
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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