Theoretical lift and damping in roll of thin wings with arbitrary sweep and taper at supersonic speeds, supersonic leading and trailing edges.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Theoretical lift and damping in roll of thin wings with arbitrary sweep and taper at supersonic speeds, supersonic leading and trailing edges


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Harmon, S.M. (author) / Jeffreys, I. (author)


    Publication date :

    1950


    Size :

    49 pages


    Remarks:

    Diagrs, Charts


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :