Effect of variations and directions and velocity of current on wind tunnel tests; case of rotating wings.
Report from German Aeronautical Experiment Station of Adlershof, near Berlin, presenting theoretical mathematical discussion of method of determining distribution of lift on airplane wings in slightly non-homogeneous air current, based on Prandtl equations
Auftriebsverteilung und daraus abgeleitete Groessen fuer Tragfluegel in schwach inhomogenen Stromungen
Luftfahrtforschung ; 16 , n 3
1939
6 pages
Article (Journal)
German
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Report for German Aeronautical Experiment Station of Adlershof near Berlin
Engineering Index Backfile | 1936
|Engineering Index Backfile | 1939
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