As part of the Quiet Clean Short-Haul Experimental Engine Program, model tests were conducted to determine the effects of thrust reverser geometric parameters on noise and reverse thrust. The acoustic tests used a 1/6 scale model thrust reverser while the aerodynamic performance tests used a 1/12 scale model reverser. Parameters which were varied in both tests include blocker spacing, blocker height, lip angle, and lip length. The impact of these parameters on peak sideline noise and reverse thrust performance is discussed.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Acoustics and aerodynamics of over-the-wing thrust reversers


    Beteiligte:
    Stimpert, D. L. (Autor:in) / Ammer, R. C. (Autor:in)


    Erscheinungsdatum :

    1976-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Asymmetric Thrust Reversers

    Chandler, Jesse M. / Suciu, Gabriel L. | NTRS | 2018


    Clocked Thrust Reversers

    Suciu, Gabriel L. / Chandler, Jesse M. | NTRS | 2017


    ASYMMETRIC THRUST REVERSERS

    CHANDLER JESSE M / SUCIU GABRIEL L | Europäisches Patentamt | 2015

    Freier Zugriff

    Clocked thrust reversers

    SUCIU GABRIEL L / CHANDLER JESSE M | Europäisches Patentamt | 2017

    Freier Zugriff