The Air Force Flight Dynamics Laboratory plans to test an advanced composite wing with an internally blown jet flap on a low cost, low risk unmanned vehicle. This technical report identifies required modifications to the BQM-34F target vehicle, including the engine and wing interface constraints, to support the flight test program. Emphasis was given to the fuselage structure, elevator control power, bleed air valve and ducting, flight control system, vehicle electrical system, and the instrumentation and telemetry systems. AFFDL provided the wing definition and jet flap wind tunnel test data.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Composite Maneuver Augmentation (COMMA) For Fighter Aircraft: Preliminary Design Study


    Contributors:

    Publication date :

    1974


    Size :

    314 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Maneuver and buffet characteristics of fighter aircraft

    Ray, E. J. / Mckinney, L. W. / Carmichael, J. G. | NTRS | 1973


    Maneuver and buffet characteristics of fighter aircraft

    Ray, E. J. / Mckinney, L. W. / Carmichael, J. G. | NTRS | 1972


    Maneuver and Buffet Characteristics of Fighter Aircraft

    E. J. Ray / L. W. Mckinney / J. G. Carmichael | NTIS | 1973


    Maneuver and buffet characteristics of fighter aircraft

    Ray, Edward J. / MacKinney, Linwood W. / Carmichael, Julian G. | TIBKAT | 1973