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.
Supersonic Transport Optimization to Mach 4
2021-01-01
Report
No indication
English
Materials for the mach 3 supersonic transport
NTRS | 1964
|Investigation of structural concepts for mach 3 + supersonic transport wing
Engineering Index Backfile | 1963
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