Simulation of aircraft using airborne V/STOL simulator is described; program was undertaken to assess influence on handling qualities of backlash and flexibility in various locations in control systems, and various realistic stability augmentation failures in presence of these backlashes; tests were completed before actual aircraft flew and, in addition to providing Canadair with data on backlashes, familiarized company pilots with flying and control system characteristics to be expected.


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    Titel :

    Simulation of Canadair CL-84 tilt-wing aircraft using airborne V/STOL simulator


    Weitere Titelangaben:

    Canada. Nat Research Council -- Aeronautical Report


    Beteiligte:
    McGregor, D.M. (Autor:in)


    Erscheinungsdatum :

    1965


    Format / Umfang :

    33 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Canadair tilt-wing/deflected slipstream V/STOL prototype program

    Phillips, F.C. | Engineering Index Backfile | 1964


    The CANADAIR CL-84 Tilt Wing Design

    Sullivan, T. M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 1993


    The Canadair CL-84 tilt wing design

    Sullivan, T. | AIAA | 1993


    Forward Swept Tilt Wing V/STOL Aircraft

    SAE / American Helicopter Society / AIAA | British Library Conference Proceedings | 1997


    Forward Swept Tilt Wing V/STOL Aircraft

    SAE / American Helicopter Society / AIAA | British Library Conference Proceedings | 1997