Interpreting high angles of attack as those associated with stall and post-stall behaviour, the report reviews both aerodynamic and dynamic aspects. Dynamic considerations include stability and control response, and pre-stall and post-stall behaviour. Aerodynamic considerations range over a wide field covering two-dimensional stall characteristics, finite wing stall characteristics, including the effects of stall control devices, downwash at high angles, aircraft configuration force and moment characteristics, and aerodynamic derivative characteristics. Unsteady effects, Mach number effects, and propeller slipstream effects are included. (Author)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Problems of Aircraft Behaviour at High Angles of Attack


    Contributors:

    Publication date :

    1969


    Size :

    117 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





    Captive Aircraft Testing at High Angles of Attack

    R. W. Butler / J. P. Christopher | NTIS | 1981


    Longitudinal motions of aircraft involving high angles of attack

    Thomas, H. H. B. M. / Collingbourne, Joan R. | TIBKAT | 1974


    Longitudinal Motions of Aircraft Involving High Angles of Attack

    H. H. B. M. Thomas / J. Collingbourne | NTIS | 1974