Precompression fin for axisymmetric inlet on winged high speed v

Details Precompression fin for axisymmetric inlet on winged high speed v Precompression fin for axisymmetric inlet on winged high speed v

1978-08-02

1981-01-06

Kelmachter, Barry L.

Aeronautics and astronautics

Aircraft power plants

102 341, 137 151, 244 1N, 244 91, B64D 2720

Patent

active

042431883

ABSTRACT:
Precompression fins extending perpendicular from the wings of a high speed missile are judiciously located relative to an axisymmetric inlet of an airbreathing power plant such that the outwash angle induced by the body and wing of the missile enhances the performance of the inlet.

REFERENCES:
patent: 2997256 (1961-08-01), Walker
patent: 3161019 (1964-12-01), Keenan et al.
patent: 3270990 (1966-09-01), Webb

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