Aerodynamically contoured, low drag wing, engine and engine nace

Details Aerodynamically contoured, low drag wing, engine and engine nace Aerodynamically contoured, low drag wing, engine and engine nace

1980-12-22

1984-05-22

Frankfort, Charles E.

Aeronautics and astronautics

Aircraft structure

Details

244 55, 244 53R, B64D 2902

Patent

active

044496826

ABSTRACT:
A nacelle mounted directly to and below a wing so as to extend forwardly therefrom. The wing has a critical zone, which includes an area in the airstream flow about the wing where either of the following conditions occur:

REFERENCES:
patent: 3199813 (1965-08-01), Roper
patent: 3658279 (1972-04-01), Robertson
patent: 3799476 (1974-03-01), Bouiller et al.
Goodmanson et al., "Recent Advances . . . for Transport Aircraft", AIAA 9th Annual Meeting, Jan. 8-10, 1973, p. 11.
Wells et al., "Wind Tunnel . . . Investigation of Over-The-Wing Propulsion/Air Frame Interferences for a Shorthaul Aircraft . . . ", NASA Contractor Report CR-2905, Sep. 1977, p. 24.

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