Assuming lifting line theory, expressions for velocity induced by walls at points along span of wing are derived for symmetrical airfoils with arbitrary lift distribution; calculations extended to unsymmetrical airfoils and to airfoils placed above or below center line of tunnel. Supplement to Report AR-7. (See Engineering Index 1951 p 1299).


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    Titel :

    Wall interference in wind tunnels of closed rectangular section: development of equations


    Weitere Titelangaben:

    Canada. Nat Research Council -- Aeronautical Report


    Beteiligte:
    Sanders, J. (Autor:in) / Pounder, J.R. (Autor:in)


    Erscheinungsdatum :

    1951


    Format / Umfang :

    26 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Wall interference in closed type wind tunnels

    Higgins, G.J. | Engineering Index Backfile | 1927


    Interference corrections for asymmetrically loaded wings in closed rectangular wind tunnels

    Garner, H. C. / Acum, W. E. A. / Großbritannien, Aeronautical Research Council | TIBKAT | 1957


    Interference corrections for asymmetrically loaded wings in closed rectangular wind tunnels

    Garner, Henry Clifford ;Acum, Wilfred Ethelbert Alfred | SLUB | 1957