Ejector ramjet

Power plants – Reaction motor – Including mechanical air compressor or air flow inducing means

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602701, F02K 712

Patent

active

053277210

ABSTRACT:
An improved ejector ramjet includes a nozzle and propulsion duct. The nozzle has first and second sides, which are preferably two-dimensional, and produces a primary fluid jet which causes secondary fluid to be entrained in the propulsion duct. The primary jet is oscillated providing energy exchange between the primary and secondary fluids in the propulsion duct in a substantially non-viscous fashion.

REFERENCES:
patent: H1007 (1982-01-01), Schadow et al.
patent: 3046732 (1962-07-01), Foa
patent: 3143856 (1964-08-01), Hausmann
patent: 3279185 (1966-10-01), Lewis et al.
patent: 3357191 (1967-12-01), Berner
patent: 3925982 (1975-12-01), Mueller
patent: 4030289 (1977-06-01), Kampe
patent: 4257224 (1981-03-01), Wygnanski
Newton, Jr. et al., "Experiments on the Interaction of Secondary Injectants and Rocket Exhaust for Thrust Vector Control", Jet Propulsion Laboratory, California Institute of Technology (1962).

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