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    Air admixture to exhaust jets (1953)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: 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.
    Type: NACA-TM-1357
    Format: application/pdf
    Location Call Number Expected Availability
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