Aerodynamic characteristics of 24 airfoils are given for speeds of 0. 5, 0.65, 0.8, 0.95 and 1.08 times speed of sound as measured in openjet air stream using models of 1-in. chord; nine members of Standard R.A.F. airfoil used by Army and Navy for propeller design, and five members of Clark Y family differing only in thickness tested; R.A.F. family in which position of maximum ordinate is varied; combined groups; group consisting of three geometrical forms, flat plate, wedge, and segment of right circular cylinder.


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    Title :

    Aerodynamic characteristics of twenty-four airfoils at high speeds


    Additional title:

    Nat. Advisory Committee Aeronautics -- Report


    Contributors:
    Briggs, L.J. (author) / Dryden, H.L. (author)


    Publication date :

    1929


    Size :

    32 pages


    Remarks:

    45 Figs.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



    Aerodynamic characteristics of twenty-four airfoils at high speeds

    Briggs, L. J. / Dryden, H. L. | TIBKAT | 1929


    Aerodynamic characteristics of airfoils at high speeds

    Briggs, L.J. / Hull, G.F. / Dryden, H.L. | Engineering Index Backfile | 1925


    Aerodynamic characteristics of airfoils at high speeds

    Briggs, L. J. / Hull, G. F. / Dryden, H. L. | TIBKAT | 1928


    Aerodynamic Characteristics of Airfoils at High Speeds

    Briggs, L J / Hull, G F / Dryden, H L | NTRS | 1925