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THE FLIGHT TEST OF TWIN-SPOOL TURBOJET ENGINE SIMULATING THE INGESTION OF MISSILE EXHAUST
Zuo Hanzhong
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 1987, (8): 436 -440 . 

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All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341