INFLUENCE OF INITIAL TEMPERATURE IRREGULARITIES AND AIR-TO-FUEL RATIO IN AFTERBURNER GTE ON SPECIFIC NOZZLE THRUST

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GRUZDEV, VN
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IZVESTIYA VYSSHIKH UCHEBNYKH ZAVEDENII AVIATSIONAYA TEKHNIKA | 1985年 / 02期
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V [航空、航天];
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08 ; 0825 ;
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页码：21 / 24
页数：4
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