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Chinese Journal of Aeronautics
1000-9361
1991 Issue 1
NUMERICAL METHOD FOR SOLVING THE EULER EQUATION FOR UNSTEADY TRANSONIC FLOWS OVER OSCILLATING AIRFOILS
Li FengweiNorthwestern Polytechnical University
..............
page:1-10
A UNIFIED APPROXIMATE FEEDBACK SOLUTION OF COPLANAR VARIABLE-SPEED INTERCEPTION GAMES
Liu Changyou and Zhang SiyingNortheast University of Technology
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page:11-19
THE FUZZY SYNTHETIC JUDGEMENT OF CORRELATING PARAMETER OF FIGHTER DESIGN
Cui Hong and Zao YongBeijing University of Aeronautics and Astronautics
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page:20-25
NUMERICAL CALCULATIONS OF GASEOUS REACTING FLOWS IN A MODEL OF GAS TURBINE COMBUSTORS
Yan Chuanjun;Tang Ming;Zhu Huiling and Sun HuixianNorthwestern Polytechnical University
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page:26-34
A REVERSED-FRAME NORMALIZATION DESIGN OF ROBUST FLIGHT CONTROL SYSTEM
Jiang Changsheng;Shen Chunlin and Hu ZhonghanNanjing Aeronautical Institute
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page:35-45
AN ANALYSIS OF THE COST-EFFECTIVENESS OF AIR DEFENSE SURVEILLANCE RADARS
Li NengjingPLA Air Force Radar Research Institute
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page:46-56
A FUNDAMENTAL STUDY OF CH-202M POLYMER QUENCHANT IN THE QUENCHING OF STEEL PARTS
Wang Yulin;Teng Lixia and Gu GuanghouNanjing Aeronautical Institute
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page:57-64
ERROR ESTIMATION AND DOUBLE MESH FOR RIGID-VISCOUS-PLASTIC FINITE ELEMENT ANALYSIS OF UNSTEADY EXTRUSION PROCESSES
Guo YongmingNanjing Aeronautical Institute
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page:65-72
ACTA AERONAUTICA ET ASTRONAUTICA SINICA
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page:73-86