Cambered wing was tested in transonic wind tunnel with indented and nonindented body, and similar plane wing with indented body; conical camber reduced and delayed wing tip stall and reduced severity of its associated longitudinal instability; other results.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Transonic aerodynamic loading characteristics of wing-body-tail combination having 52.5° sweptback wing of aspect ratio 3 with conical wing camber and body indentation for design mach number of root 2


    Additional title:

    NASA -- Tech Note


    Contributors:
    Cassetti, M.D. (author) / Re, R.J. (author) / Igoe, W.B. (author)


    Publication date :

    1961


    Size :

    99 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :