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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Additional title:

    SAE -- Paper


    Contributors:

    Conference:

    SAE Meeting ; 1966



    Publication date :

    1966


    Size :

    15 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :



    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