The variable stream control engine is determined to be the most promising propulsion system concept for advanced supersonic cruise aircraft. This concept uses variable geometry components and a unique throttle schedule for independent control of two flow streams to provide low jet noise at takeoff and high performance at both subsonic and supersonic cruise. The advanced technology offers a 25% improvement in airplane range and an 8 decibel reduction in takeoff noise, relative to first generation supersonic turbojet engines.


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    Title :

    Advanced supersonic propulsion study, phase 3


    Contributors:
    Howlett, R. A. (author) / Johnson, J. (author) / Sabatella, J. (author) / Sewall, T. (author)

    Publication date :

    1976-12-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






    Advanced Supersonic Propulsion Study, Phase 3

    R. A. Howlett / J. Johnson / J. Sabatella et al. | NTIS | 1976


    Advanced supersonic propulsion study

    Sabatella, J. A. | NTRS | 1974


    Advanced Supersonic Propulsion Study

    J. A. Sabatella | NTIS | 1974