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
01.07.1947
Sonstige
Keine Angabe
Englisch
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
| Engineering Index Backfile | 1953