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Inverse Design Analysis Method on Rotor with Advanced Aerodynamic Configuration Based upon Target Pressure Distribution
ZHAO Guoqing, ZHAO Qijun
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2014, (3): 744 -755 .  DOI: 10.7527/S1000-6893.2013.0267

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Total visits: 6658907 Today visits: 1341All copyright © editorial office of Chinese Journal of Aeronautics

All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341