Three proposed SCAR propulsion systems in terms of aircraft range for a fixed payload and take-off gross weight with a design cruise Mach number 2.7 are evaluated. The effects of various noise and operational restraints are determined and sensitivities to some of the more important performance variables are presented for the most probable design noise and operational restraint case. Critical areas requiring new or improved technology for each cycle are delineated. (Author)


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    Title :

    Assessment of Variable-Cycle Engines for Mach 2.7 Supersonic Transports


    Contributors:
    S. J. Morris (author) / W. E. Foss (author) / J. W. Russell (author)

    Publication date :

    1976


    Size :

    59 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Assessment of Variable-cycle Engines for Mach 2.7 Supersonic Transports

    Morris, S. J. / Foss, W. E., Jr. / Russell, J. W. | NTRS | 1976


    Variable Cycle Engines for Advanced Supersonic Transports

    Kozlowski, Hilary / Howlett, Robert A. | SAE Technical Papers | 1975


    Variable cycle engines for advanced supersonic transports

    Howlett, R. A. / Kozlowski, H. | NTRS | 1975