Two-dimensional inlet for a high speed winged flight vehicle

Details Two-dimensional inlet for a high speed winged flight vehicle Two-dimensional inlet for a high speed winged flight vehicle

1978-08-02

1981-01-20

Kelmachter, Barry L.

Aeronautics and astronautics

Aircraft power plants

137 151, 244 15, B64D 3302

Patent

active

042458030

ABSTRACT:
For a winged high speed missile that includes a two-dimensional inlet supplying air to the missile power plant, the compression ramp of the inlet is oriented with respect to the outwash angle produced by the missile body and the underneath surface of the wing such that the compression ramp of the inlet is subjected to an effective angle of attack. By proper inlet orientation the captured flow is turned inwardly toward the missile center line further compressing the incoming air.

REFERENCES:
patent: 2596435 (1952-05-01), Robert
patent: 2990142 (1961-06-01), Ferri
patent: 2997256 (1961-08-01), Walker

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