This report presents an analysis of results of wind-tunnel tests conducted at the D.V.L. Values were determined for the effectiveness of all the controls at various angles of attack. The autorotation was studied by subjecting the rotating model to an air blast.
Analysis of flight and wind-tunnel tests on Udet airplanes with reference to spinning characteristics
1929-03-01
Miscellaneous
No indication
English
Engineering Index Backfile | 1929
|Engineering Index Backfile | 1929
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