Stabilized aero-optical free shear layer interface

Aeronautics and astronautics – Miscellaneous

Patent

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Details

2441291, 244130, 244207, 372104, 359509, 359894, B64C 2104

Patent

active

050693972

ABSTRACT:
In an aero-optical interface for an aircraft optical aperture, the separation of the upstream boundary layer from the edge of the aperture creates a region of turbulance which persists downstream over the full area of the aperture. This invention promotes an early develpment of a steady velocity profile at the upstream aperture edge which is approximately the same as a stable, self-similar shear flow velocity profile over the entire aperture. This is accomplished by thickening the boundary layer upstream of the aperture, and blowing a curtain of air across the aperture from its upstream edge at the point of separation of the boundary flow. This produces a shear flow region foot that causes the overall velocity profile to be equal to a stable self-similar free shear layer.

REFERENCES:
patent: 2049573 (1936-08-01), Stalker
patent: 2219234 (1940-10-01), Messerschmitt
patent: 2430431 (1947-11-01), Lanier
patent: 2841182 (1958-07-01), Scala
patent: 2841344 (1958-07-01), Stroukoff
patent: 2894703 (1959-07-01), Hazen
patent: 3216455 (1965-11-01), Cornell et al.
patent: 3360221 (1967-12-01), Heskestad
patent: 3374971 (1968-03-01), Heskestad
patent: 3437371 (1969-04-01), Gallie
patent: 3836237 (1974-09-01), Egan et al.
patent: 3934846 (1976-01-01), Maurer
patent: 3951360 (1976-04-01), Anyonnaz
patent: 3973218 (1976-08-01), Kepler et al.
patent: 3973219 (1976-08-01), Kepler et al.
patent: 4664345 (1987-05-01), Lurz
patent: 4703904 (1987-11-01), Haslund
Buell, "Airloads Near the Open Port of a One-Meter Airborne Telescope", AIAA Paper 75-71, Jan. 20-22, 1975.
Boeing Doc. No. D-180-28729, "Free Shear Layer Aero-Optic Jitter", P. Cassady, Apr. 1985.
Boeing Doc. No. D-180-28220-1, "Angular Deflection of a Light Ray Through a Free Shear Layer", P. Casady, Apr. 1985.
Boeing Doc. No. D-180-28219-1, "Compressible Turbulent Shear Layer Growth Over Optical Ports", P. Cassady, Apr. 1985.

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