Supervised by： China Aerospace Science and Technology Corporation
Sponsored by： China Academy of Aerospace Aerodynamics
Chinese Society of Astronautics
China Aerospace Publishing House Co., LTD

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Experimental Study of the Parameters Influence on Flow Characteristic of the Three-Electrode Plasma Synthetic Jet Actuator
WANG Lin, LUO Zhen-bing, XIA Zhi-xun, ZHOU Yan, DENG Xiong
2017, 2(6): 1-8. DOI: 10.19527/j.cnki.2096-1642.2017.06.001
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Operating Characteristic of the Horizontal Momentum Injection Actuator of Plasma Synthetic Jet
ZHANG Yu-chao, TAN Hui-jun, CHENG Lin, HE Xiao-ming, HUANG He-xia, ZHUANG Yi, ZHANG Yue
2017, 2(6): 9-17. DOI: 10.19527/j.cnki.2096-1642.2017.06.002
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Active Control of Low Reynolds Number Airfoil Flow by Implicit Large Eddy Simulation
ZHU Yu-jie, SUN Zhen-sheng, ZHANG Wei, ZHANG Shi-ying
2017, 2(6): 18-27. DOI: 10.19527/j.cnki.2096-1642.2017.06.003
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Aerodynamic Interference Between Dual Wings in Transonic Box-wing Aircraft
ZHUO Mei-fang, JIANG Chong-wen, LEE Chun-hian
2017, 2(6): 28-38. DOI: 10.19527/j.cnki.2096-1642.2017.06.004
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Droplet Impingement Characteristics with Dual Synthetic Jet Control
JIANG Hao, XIA Zhi-xun, LUO Zhen-bing, DENG Xiong, YANG Sheng-ke, LIU Qiang
2017, 2(6): 39-47. DOI: 10.19527/j.cnki.2096-1642.2017.06.005
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Numerical Study on Aerodynamic Loads of a High-speed Aircraft Folding Wing in Its Deploying Procedure
FAN Guo-fang, LI Qiang, CAO Xiao-long, LUO Jin-ling
2017, 2(6): 48-53. DOI: 10.19527/j.cnki.2096-1642.2017.06.006
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Factors in Calculating Heat Flux on the Shoulder of Apollo Like Reentry Capsule
DING Zhong-hang, WU Song-ping
2017, 2(6): 54-63. DOI: 10.19527/j.cnki.2096-1642.2017.06.007
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