Downwash Characteristics and Vortex-Sheet Shape Behind 63° Swept-Back Wing-Fuselage Combination at Reynolds Number of 6.1 × 106.
Downwash characteristics and vortex-sheet shape behind 63° swept-back wing-fuselage combination at Reynolds number of 61 × 106
NACA -- Tech Note
1954
45 pages
Report
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
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
|