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Supersonic Transport Optimization to Mach 4 Commercially viable supersonic transports require solution spaces to a longish list of serious issues including high drag, heating, emissions, costs, weights, acoustics, etc. Report addresses potential approaches to these issues including drag reduction, flow control, propulsion/ fuels/energetics, and synergistic frontier aircraft configurations across the board proffering large increases in lift to drag ratio.
Document ID
20205011829
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Dennis M Bushnell
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
December 28, 2020
Publication Date
January 1, 2021
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA/TM-20205011829
Funding Number(s)
WBS: 736466.01.01.07.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
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