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Li NONG, Zishuai SHENG, Jun XIAN, Huaibao ZHANG.
Numerical simulation of separated flow around iced airfoil based on high⁃order schemes
[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S2): 729291-729291.
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Yatian ZHAO, Zhiyuan SHAO, Chao YAN, Xinghao XIANG.
Comparative analysis of Reynolds stress and eddy viscosity models in separation flow prediction
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(11): 127619-127619.
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WEI Ziyan, LI Jie, ZHANG Heng, YANG Zhao.
Improved aerodynamic design of laminar wing section of laminar verifying aircraft
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(11): 526760-526760.
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ZHANG Heng, LI Jie, GONG Zhibin.
Numerical simulation of separated flow around a multi-element airfoil at high angle of attack with iced slat
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(2): 520733-520746.
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XU Xiao, YUE Lianjie, LU Hongbo, XIAO Yabin, ZHANG Xinyu.
Flow characteristics of hypersonic inlet starting with diaphragm rupture
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(6): 1795-1804.
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Lu Xi-yun;Zhuang Li-xian;Yin Xie-yuan;Tong Bing-gang.
NUMERICAL SIMULATION OF FLOWS PAST A LONGITUDINALLY OSCILLATING AIRFOIL AT HIGH INCIDENCES
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1993, 14(11): 632-635.
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Li Feng;Wang Yi-yun;Cui Er-jie.
AERODYNAMIC INVESTIGATION ON INTERACTION OF VORTEX WITH STATIONARY AIRFOIL
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1993, 14(11): 625-628.
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Zhou Wei-jiang;Ma Han-dong;Ma Yan-wen.
NUMERICAL STUDY OF SUPERSONIC FLOW OVER A BACKWARD STEP WITH TRANSVERSE INJECTION
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1993, 14(1): 14-19.
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Xu Cheng;Zhang Shi-ying;Zhou Ming-de.
A PRELIMINARY INVESTIGATION OF THE CONTROL OF SEPARATED FLOW BY MEANS OF EXCITATION
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1993, 14(1): 72-75.
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Lu Xi-yun;Yin Xie-yuan;Zhuang Li-xian.
NUMERICAL SIMULATION OF FLOWS AROUND OSCILLATING AIRFOIL AT LARGE INCIDENCES
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1992, 13(11): 571-576.
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Yun Qilin;Zhao Changan.
MEASUREMENT OF TURBULENT BOUNDARY LAYER IN TRANSONIC FLOW
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1991, 12(11): 563-567.
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Huang Xijun;Dong Jinzhong;Xiao Chengshu.
INVESTIGATION ON VORTEX CONTROL TECHNIQUE OF FLOW SEPARATION IN DIFFUSER
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1991, 12(10): 464-469.
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Yuan Li;Lu Zhiyong;Wu Jianmin.
CALCULATION OF UNSTEADY AERODYNAMIC LOADS ON WINGS WITH AN OSCILLATORY LEADING EDGE FLAP
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1990, 11(9): 515-520.
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Feng Yanan;Xia Xuejian;Liu Rizhi.
THE EFFECT OF THE NOSE SHAPE AND WING LOCATION TOWARD THE WING VORTEX BREAKDOWN
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1990, 11(12): 588-591.
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Tang Dengbin.
AN INVESTIGATION OF UNSTEADY LEADING EDGE SEPARATION OF RAPIDLY PITCHED AIRFOILS
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1989, 10(5): 279-283.
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