NASA NTRS · 19930093873
Air admixture to exhaust jets
Abstract
The problem of thrust increase by air admixture to exhaust jets of rockets, turbojet, ram- and pulse-jet engines is investigated theoretically. The optimum ratio of mixing chamber pressure to ambient pressure and speed range for thrust increase due to air admixture is determined for each type of jet engine.
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Sanger, Eugen. 1953-07-01. Air admixture to exhaust jets. https://ntrs.nasa.gov/citations/19930093873
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