Limited test program is being conducted on prototype of Canadair CL-84 tilt-wing V/STOL aircraft to evaluate its stability and control design objectives; results indicate that only very minor modifications were necessary with regard to flying control criteria previously established through analysis, fixed-base simulator studies, and variable-stability helicopter tests; qualitative assessment made thus far of handling qualities of CL-84 has proven adequacy of established criteria for stability and control performance for systems as complex as that of CL-84.


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    Titel :

    Report on stability and control testing of tilt wing V/STOL aircraft


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:

    Kongress:

    SAE Meeting ; 1966



    Erscheinungsdatum :

    1966


    Format / Umfang :

    15 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    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



    Design aspects and flight testing vertol 76 tilt-wing VTOL/STOL research aircraft

    Dancik, P.J. / Peck, W.B. | Engineering Index Backfile | 1958