This report presents comprehensive pressure-distribution measurements on four (4) swept-back wings (phi = 0 deg, 15 deg, 30 deg, and 45 deg) of constant chord and over a large range of angles of attack with symmetrical air flow. The distributions, experimentally obtained, were compared with theoretical ones calculated by the methods of Weissinger and Multhopp.
Pressure-Distribution Measurements on Unyawed Swept-Back Wings
1947-07-01
Miscellaneous
No indication
English
Pressure-distribution measurements on unyawed swept-back wings
TIBKAT | 1947
|Pressure-distribution measurements on unyawed swept-back wings
Engineering Index Backfile | 1947
|Lift distribution of swept-back wings
Engineering Index Backfile | 1947
|The lift distribution of swept-back wings
TIBKAT | 1947
|Structural Aspects of Swept-Back Wings
Emerald Group Publishing | 1953
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