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SASURIE ... through the nozzle, the exit velocity Ve can be expressed in terms of inlet and outlet pressure ... The condition of gas in a combustion chamber at entry are M1=0.28, T01=380 K,.. by H Cai · Cited by 3 — International Journal of Aerospace Engineering ... without considering the influence of internal combustion state on exhaust plume flow field characteristics.. Exhaust gas velocity — Some typical values of the exhaust gas velocity Ve for rocket engines burning various propellants are: 1.7 to 2.9 ... 3a5286bf2b 42
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