Calculating pressure distribution round ailfoil at any angle of incidence below stalling point from known distribution at any are angle of incidence; knowledge is becoming of increasing importance in naval architecture, applying to streamline rudders and propeller-blade sections. (See also Mar. Engr. and Motorship Bldr., vol. 54, no. 644, May 1931, p. 198)


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    Title :

    Calculation of pressure distribution on airfoils


    Additional title:

    Uebertragung der Druckverteilung an einem Tragfluegelprofil bei einem bestimmten auf einen beliebigen Anstellwinkel


    Contributors:
    Weinig, F. (author)

    Published in:

    Werft-Reederei-Hafen ; 12 , n 7 ; p 115-116


    Publication date :

    1931


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    German


    Keywords :


    Calculation of pressure distribution on airfoils

    Weinig, F. | Engineering Index Backfile | 1931


    Transonic Airfoils with a Given Pressure Distribution

    HASSAN, A. / SOBIECZKY, H. | AIAA | 1981


    Pressure distribution over airfoils at high speeds

    Briggs, L. J. / Dryden, H. L. | TIBKAT | 1926


    Pressure distribution over airfoils with fowler flaps

    Wenzinger, C.J. / Anderson, W.B. | Engineering Index Backfile | 1938


    Pressure distribution over airfoils with Fowler flaps

    Wenzinger, Carl J. / Anderson, Walter B. | TIBKAT | 1938