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 Nat Advisory Committee Aeronautics -- Tech Memo n 751 Aug 1934 10 p 5 supp plates)
Untersuchung von Reibungsschichten am Flugzeug
Untersuchung von Reibungsschichten am Flugzeug
Luftfahrtforschung ; 11 , n 1
1934
7 pages
Aufsatz (Zeitschrift)
Deutsch
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Untersuchung von Reibungsschichten am Flugzeug
Engineering Index Backfile | 1934
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