Variable-throat chin inlet high Mach number missile application

Fluid handling – Processes – Cleaning – repairing – or assembling

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244 53B, F02C 7042

Patent

active

051672499

ABSTRACT:
Variable chin-inlet for a missile wherein radially movable compression ramps vary the throat area so as to compress flow in the plane of the upstream boundary layer growth.

REFERENCES:
patent: 3011307 (1961-12-01), Edelfelt
patent: 3080707 (1963-03-01), Vetter
patent: 3265331 (1966-08-01), Miles
patent: 4132240 (1979-01-01), Frantz
patent: 4372505 (1983-02-01), Syberg
Variable-Geometry Intake; Flight; May 18, 1967; p. 812.

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