Downwash Characteristics and Vortex-sheet Shape Behind a 63 Degree Swept-back Wing-fuselage Combination at a Reynolds Number of 6.1 x 10(exp 6)
1954-05-01
Miscellaneous
No indication
English
Engineering Index Backfile | 1954
Prediction of downwash behind swept-wing airplanes at subsonic speed
Engineering Index Backfile | 1955
|The Downwash Field behind a swept wing at low speed
TIBKAT | 1968
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