Report deals with development of method which gives lucid and convenient solution of low conditions in vicinity of common, thick airfoil section wherein thickness of profile is taken into account. Bibliography. From Jahrbuch 1938 der Deutschen Luftfahrtforschung.


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    Title :

    Two-dimensional potential flow past ordinary thick wing profile


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Memo


    Contributors:
    Keune, F. (author)


    Publication date :

    1942


    Size :

    51 pages


    Remarks:

    9 Supp sheets


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Subsonic gas flow past wing profile

    Christianovich, S.A. / Yurev, I.M. | Engineering Index Backfile | 1950


    Modelling of Flow Past Body with Thick Wake in Classical Air Wing Theory

    Toison, F. / Legallais, P. / Hureau, J. | British Library Online Contents | 1996


    Modelling of Flow Past Body with Thick Wake in Classical Air Wing Theory

    Toison, F. / Legallais, P. / Hureau, J. et al. | British Library Conference Proceedings | 1996



    Scale Effect at Transonic Flow Past a Swept Thick Supercritical High-Aspect-Ratio Wing

    Bokser, V. D. / International Council of Aeronautical Sciences | British Library Conference Proceedings | 1994