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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Acoustics and aerodynamics of over-the-wing thrust reversers


    Contributors:


    Publication date :

    1976-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Asymmetric Thrust Reversers

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


    Clocked Thrust Reversers

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


    Clocked thrust reversers

    SUCIU GABRIEL L / CHANDLER JESSE M | European Patent Office | 2017

    Free access

    ASYMMETRIC THRUST REVERSERS

    CHANDLER JESSE M / SUCIU GABRIEL L | European Patent Office | 2015

    Free access