Investigation to determine severity of dynamic stability and control problems; force and tuft tests made to determine static stability and wing stall characteristics, and calculations made to determine boundary of zero damping of lateral oscillation.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Flight tests of airplane model with 62° swept-back wing in Langley free-flight tunnel


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Maggin, B. (author) / Bennett, C.V. (author)


    Publication date :

    1947


    Size :

    14 pages


    Remarks:

    10 Supp plates, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :