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Engine/airframe compatibility studies for supersonic cruise aircraftEngine/airframe compatibilities are studied utilizing the advanced supersonic transport point design as the baseline for comparison. Detailed studies of four engines are given. The technical analysis, configuration descriptions, and study results are presented for each of the four specific engines studied.
Document ID
19750017844
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 3, 2013
Publication Date
May 1, 1975
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-132610-1
MDC-J4505-SUPPL
Report Number: NASA-CR-132610-1
Report Number: MDC-J4505-SUPPL
Accession Number
75N25916
Funding Number(s)
CONTRACT_GRANT: NAS1-13229
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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