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Acta Aerodynamica Sinica
FQ: 双月
AD of Publication: 四川省绵阳市
Lanuage: 中文;英文;
ISSN: 0258-1825
CN: 51-1192/TK
YP: 1980
Url: 中国空气动力学会
Recommended Journals
Acta Aerodynamica Sinica
1988 -01
Catalog
THE NUMERICAL SIMULATION OF THE 3-D VISCOUS SEPARATED FLOWS AROUND THE FLAP MOUNTED ON A FLAT PLATE Zhang Hanxing Yu Zhechu Geng Weiqun (China Aerodyamic Research and Development Center)
CALCULATION OF INTERNAL VORTEX FLOW Bian Yingui Zhao Lie Yu Xin (institute of Mechanics, Academic Sinica)
THEORETICAL INVESTIGATION OF SEPARATED VORTEX MOTION AND VORTEX BREAKDOWN FEATURE Lin Bingqiu (Beijing institute of Aerodynamics)
ON THE SECONDARY SEPARATION AND THE REDUCTION OF CIRCULATION IN THE WAKE FLOW BEHIND A CIRCULAR CYLINDER Ling Guocan (Institute of Mechanics, Chinese Academy of sciences, Beijing)
2-D INCOMPRESSIBLE SEPARATED FLOW COMPUTATION USING CONSTRAINT ITERATION Zhang Xihua (Development Department Chengdu Aircraft Co.)
VISCOUS/INVISCID INTERACTION ALGORITHM TO ANALYZE TRANSONIC AIRFOILS FLOWS WITH SEPARATION Zhang Huiliu Cao Qipeng (Nanjing Aeronautical institute)
INSTANTANEOUS CRITICAL POINT IN UNSTEADY FLOW Wu Jiezhi Jiang Linbo (Chinese Aeronautical Establishment)
THE CALCULATION OF GROUND EFFECT ON THE FLOW ABOUT AN AIRFOIL WITH REAR SEPARATION Jiang Linbo Zhu Ziqiang (Beijing institute of Aeronautics and Astronautics)
COMPUTATION OF TWO-DIMENSIONAL COMPRESSIBLE VISCOUS NOZZLE FLOW WITH SEPARATION Chen Zelin (Beijing Institute of Aerodynamics)
VORTEX SYSTEM AND PRESSURE DISTRIBUTION OF SLENDER BODIES WITH ELLIPTICAL CROSS-SECTION NOSE AT HIGH ANGLE OF ATTACK Xiong Shanwen Feng Yanan (Beijing Institute oj Aeronautics and Astronautics)
VISUALIZATION AND MEASUREMENT OF THE SPACE VORTEX SYSTEM ON SLENDER BODY Xia Xuejian Yu Xiaosheng (Beijing institute of Aeronautics and Astronautics)
THE FORMATION MECHANISM OF THE ASYMMETRIC SPATIAL VORTEX OF SLENDER BODIES AT HIGH ANGLE OF ATTACK Wang Zixing(Nanjing Aeronautical institute)Su Dai(East China institute of Technology)
AERODYNAMIC CHARACTERISTICS OF VORTEX FLAP AND ITS COMBINATION WITH APEX FLAP Zhuang Fenggan Xin Dingding Wang ZufengZhang Ziqiang Guo Wenhai (Beijing Institute of Aeronautics and Astronautics)
THE CHARACTERISTICS OF NEAR WAKE BEHIND BLUFF BODIES Ming Xiao Dai Changhui (Nanjing Aeronautical institute)
EXPERIMENTAL INVESTIGATION ON THE FORMATION MECHANISM OF THE EFFECT OF SPIN NOSE TO ASYMMETRIC VORTEXES ON SLENDER BODY AT HIGH ANGLE OF ATTACK Su Dai (East China Institute of Technology)Wang Zixing (Nanjing Aeronautical institute)
THE EXPERIMENTAL INVESTIGATION ON THE FORMATION AND DECAY OF VORTEX UNDER INTERACTION OF A JET WITH A CROSSFLOW Sheng chunhua Zhang Fengbei (Nanjing Aeronautical institute)
EXPERIMENTAL STUDIES OF UNSTEADINESS OF THE SHOCK WAVE STRUCTURE IN HYPERSONIC TURBULENT SEPARATED FLOWS Wang Shifeng Li Qingquan (institute of Mechanics, Academic Sinica)
VORTEX INTERACTION OF TWO WING-BODY MISSILE CONFIGURATIONS Feng yanan Huang Zheng (Beijing Institute of Aeronautics and Astronautics)
THE INFLUENCE ON THE POSITION OF VORTEX BREAKDOWN BY SPIRAL FORCING HARMONIC OSCILLATION Yao Minfei Jiang Linbo We Jiezhi (Chinese Aeronautical Establishment)Ma Huiyang (University of Science and Technology of China)Pan Jiyuan Huang Zheng (Beijing Institute of Aeronautics and Astronautics)Cai Huijuan Huang Xingzhong (Beijing Institute of Aeronautics)
EFFECT OF GAP SIZE ON HYPERSONIC SEPARATED FLOW Gao Ruifeng (China Aerodynamic Research and Development Center)
THE MOVEMENT OF LARGE SCALE EDDIES IN TURBULENT WALL FLOW AND TURBULENT MODEL Yang Xini (Beijing institute of Aerodynamics)
CHARACTERISTICS OF ASYMMETRIC VORTICES AND METHODS TO ALLEVIATE OFF-PLANE FORCES AND MOMENTS Zeng Guangcun Qin Yixian Ding Qingguo Yuan Youxin (Beijing Institute of Aerodynamics)
1988 Issues:  [01] [02] [03] [04]
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