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THEORETICAL SPECIFIC IMPULSE FOR TWO-PHASE FLOW IN NOZZLE OF ROCKET-RAMJET ENGINE——A SIMPLE ESTIMATION METHOD
Bi Shiguan
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 1983, (4): 101 -104 . 

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All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341