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.


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    Title :

    Supersonic Transport Optimization to Mach 4


    Contributors:

    Publication date :

    2021-01-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





    Turbojet and turbofan engines for a mach 3 supersonic transport

    Dugan, J. F., Jr. / Koenig, R. W. / Mc Auliffe, T. B. et al. | NTRS | 1964



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    Van Dyke, Jr., J.D. | Engineering Index Backfile | 1963