Investigation of boundary layers on airplane wing in free flight; equipment and method developed for recording boundary layers on surface of airfoil in wind tunnel; results are in close agreement with wind-tunnel tests of other experimenters; observations on transition from laminar to turbulent flow check with other tests and calculations. (See also Luftfahrtforschung v 11 n 1 May 15 1934 p 26-32)
Untersuchung von Reibungsschichten am Flugzeug
Untersuchung von Reibungsschichten am Flugzeug
1934
10 pages
5 Supp plates
Report
English
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Untersuchung von Reibungsschichten am Flugzeug
Engineering Index Backfile | 1934
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