Wind-tunnel tests of a simplified nacelle on a semispan wing having approximately 35 degrees of sweepback were made at low speeds to evaluate the effects of the nacelle on the aerodynamic characteristics of the wing. Force, moment, and pressure-distribution measurements are presented for the nacelle underslung and centrally mounted on the wing and mounted on a strut below the wing.
Effect of a Nacelle on the Low-speed Aerodynamic Characteristics of a Swept-back Wing
1948-07-21
Miscellaneous
No indication
English
Engineering Index Backfile | 1948
|Aerodynamic Characteristics of a Swept Augmentor Wing
NTIS | 1972
|Aerodynamic characteristics of a swept augmentor wing
NTRS | 1972
|Aerodynamic characteristics of a swept augmentor wing
NTRS | 1972
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