Characteristics of ailerons in Reports nos. 298, 343 and 370 summarized in form of empirical equations which relate aileron dimensions and displacements to rolling, yawing, and hinge moments for pitch angles of 0 and 12°, corresponding to angles of attack of wings of 4 and 16°.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Rolling, yawing, and hinge moments produced by rectangular ailerons


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Notes


    Contributors:
    Heald, R.H. (author)


    Publication date :

    1933


    Size :

    12 pages


    Remarks:

    3 Supp Sheets


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English