Test set-up and investigations to show that low-pressure field due to interruption of continuous flow, seems to be fairly independent of wing profile so far as extent and direction are concerned. (see also Zeit. fuer Flugtechnik und Motorluftschiffahrt, vol. 22, no. 10, May 28, 1931, pp. 289-300, 32 figs.)
Down-wash measurements behind wings for interrupted flow
Abwindmessungen hinter Tragfluegein mit abgerissener Stroemung
1931
6 pages
32 Figs. on Supp. plates
Report
Englisch
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