A low-speed wind-tunnel investigation was conducted in a full-scale tunnel to determine the performance and static stability and control characteristics of a large-scale model of a blended-arrow advanced supersonic transport configuration incorporating variable-cycle engines and vectoring exhaust nozzles. Configuration variables tested included: (1) engine mode (cruise or low-speed), (2) engine exit nozzle deflection, (3) leading-edge flap geometry, and (4) trailing-edge flap deflection. Test variables included values of C sub micron from 0 to 0.38, values of angle of attack from -10 degrees to 30 degrees, values of angle of sideslip, from -5 degrees to 5 degrees, and values of Reynolds number, from 3.5 million to 6.8 million. (Author)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Low-Speed Wind-Tunnel Tests of a Large Scale Blended Arrow Advanced Supersonic Transport Model Having Variable Cycle Engines and Vectoring Exhaust Nozzles


    Contributors:

    Publication date :

    1976


    Size :

    57 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English