This report presents the results of tests of 209 simple wing-fuselage combinations made in the NACA variable-density wind tunnel to provide information regarding the effects of aerodynamic interference between wings and fuselages at a large value of Reynolds number.
Interference of Wing and Fuselage from Tests of 209 Combinations in the NACA Variable-Density Tunnel
1936-01-01
Miscellaneous
No indication
English
Engineering Index Backfile | 1947
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