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AERODYNAMIC DESIGN CHARACTERISTIC OF TEST CELL FOR-HIGH. BY-PASS RATIO TURBOFAN ENGINE
Guo Shaorong
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 1987, (6): 251 -255 . 

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All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341