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
English
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