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25 November 1996, Volume 17 Issue S1

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25 November 1996, Volume 17 Issue S1

论文

TURBULENT SEPARATION FEATURES INDUCED BY BLUNT FINS IN HYPERSONIC FLOW
Abstract( 1418 )

Wang Shifen;Wang Yu

1996, (S1): 2-7.

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NAVIER STOKES CALCULATIONS OF WAKE AND GROUND VORTEX INDUCED BY A ROTOR IN FORWARD FLIGHT WITH GROUND EFFECTS
Abstract( 1922 )

Kang Ning;Sun Mao

1996, (S1): 8-13.

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NUMERICAL STUDY OF THE FLOW PATTERNS AROUND ELLIPSOIDS WITH DIFFERENT AXES RATIOS
Abstract( 1913 )

Yuan Li;Xin Dingding;Zhuang Fenggan

1996, (S1): 14-20.

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AIRBORNE PREDICTIVE LOW ALTITUDE WINDSHEAR DETECTION NUMERICAL SIMULATION
Abstract( 1456 )

Sun Qingmin;Jin Changjiang

1996, (S1): 21-25.

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DYNAM IC STALL CHARACTERS OF NACA 0012 AIRFO IL AND INVESTIGATIONS OF DYNAMIC PRESSUREM EASUREM ETHODS
Abstract( 1384 )

Xia Yushun;Xi Zhongxiang;Zhou Ruixing;Shang Guanyunxin

1996, (S1): 26-31.

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APPLICATION OF AEROSERVOELASTIC TECHNICS ON AIRFRAME DESIGN
Abstract( 1040 )

Chen Guibin;Zou Congqing

1996, (S1): 32-36.

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ADDITIONAL DISPLACEMENT METHOD FOR PREDICTION OF FATIGUE CRACK INITIATION LIVES OF METALLIC STRUCTURES BASED ON DAMAGE MECHANICS
Abstract( 1321 )

Zhao Jun;Zhang Xing

1996, (S1): 37-42.

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TRANSIENT IMPACTING RESPONSES OF BAR AND PLATE STRUCTURES
Abstract( 1268 )

Xing Yufeng;Zhu Dechao

1996, (S1): 43-47.

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UNIVERSAL DISTRIBUTION MODEL OF STRENGTH AND LIFE AND ITS TEST
Abstract( 1151 )

Dong Cong;Rong Haiwu;He Qingzhi

1996, (S1): 48-52.

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NUMERICAL SIMULATION OF INFLUENCE OF HOT SMOKE STREAM ON AIRCRAFT′S APPROACH FLIGHT
Abstract( 1372 )

Jin Changjiang;Hong Guanxin;Han Chao

1996, (S1): 53-55.

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EXPERIMENTAL INVESTIGATION OF THE VORTEX VERTICAL TAIL INTERACTION
Abstract( 1265 )

Zhou Danjie;Xia Xuejian

1996, (S1): 56-59.

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CONTROL REQUIREMENTS FOR POST STALL MANEUVERING
Abstract( 1327 )

Zhang Shuguang;Fang Zhenping

1996, (S1): 60-63.

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IDENTIFICATING THE PARAMETERS OF PILOT STRUCTURAL MODEL
Abstract( 1417 )

Qu Xiangju;Fang Zhenping

1996, (S1): 64-67.

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THE SCHEME EFFECTS OF NUMERICAL SOLUTIONS FOR SHOCK/BOUNDARY LAYER INTERACTION
Abstract( 1220 )

Yan Chao;Chen Liang

1996, (S1): 68-71.

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CALCULATION OF SUPERSONIC INVISCID FLOW OVER BLUNT NOSED BODIES
Abstract( 1374 )

Shen Xialing;Wu Zongcheng;Chen Yanqing

1996, (S1): 72-75.

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NUMERICAL SIMULATION OF SECONDARY VORTICITIES IN BLADE PASSAGE
Abstract( 1314 )

Zhou Zhenggui;Wu Guochuan

1996, (S1): 76-78.

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STABILITY PROBLEMS OF CROSSFLOW STATIONARY DISTURBANCES IN THE BOUNDARY LAYER
Abstract( 1353 )

Tang Dengbin;Cheng Guowei;Ma Qianrong

1996, (S1): 79-82.

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EFFECT OF TUNNEL WALLS ON VORTEX BREAKDOWN LOCATION OVER DELTA WINGS WITH OSCILLATING IN PITCH TO VERY HIGH ANGLES OF ATTACK
Abstract( 1682 )

Zhang Wenhua;Zhang Qingli;Zhou Xingkui

1996, (S1): 83-86.

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TWO ORDER IMPLICIT FLUX VECTOR SPLITTING SCHEMES FOR TWO DIMENSIONAL TRANSONIC VISCOUS FLOW
Abstract( 1396 )

Liu Yi;Liu Bin;Xiang Yimin

1996, (S1): 87-90.

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CLOSED FORM SOLUTION OF STRESS INTENSITY FACTORS OF THREE DIMENSIONAL FINITE BODIES CONTAINING INCLINED EMBEDDED CRACKS BY ENERGY DIFFERENCE RATE METHOD
Abstract( 1116 )

Wang Qizhi;Zhang Xing

1996, (S1): 91-94.

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NONLINEAR DYNAMIC STABILITY OF COMPOSITE LAMINATED CYLINDRICAL PANELS
Abstract( 1586 )

Qian Chun;Yang Jialing;Xi Feng

1996, (S1): 95-98.

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ELASTIC BEHAVIOUR OF 2 D AND 3 D TEXTILE STRUCTURAL COMPOSITES
Abstract( 1253 )

Yan Ying Ding Yiqiang

1996, (S1): 99-103.

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OPTIMIZATION METHOD OF THE FINITE ELEMENT DYNAMIC MODEL OF LARGE STRUCTURES
Abstract( 1136 )

Chen Mulan;Song Haiping

1996, (S1): 104-108.

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ADAPTIVE COMPOSITE CLOSED CELL THIN WALLED BEAM SHAPE CONTROL
Abstract( 1147 )

Yan Fei

1996, (S1): 109-113.

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A METHOD FOR DEVELOPING SONIC FATIGUE TEST SPECTRUM OF AIRCRAFT STRUCTURE
Abstract( 1767 )

Yao Jin

1996, (S1): 114-116.

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STUDY ABOUT RADAR CROSS SECTION OF CREEPING WAVES FOR A TWO DIMENSIONAL WING
Abstract( 1465 )

Ma Dongli;Wu Zhe

1996, (S1): 117-120.

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THE CONTRAST SUNNING EXPERIMENTS BETWEEN HONEYCOMBED PLATE SOLAR COLLECTOR AND THE COMMON COLLECTOR
Abstract( 2126 )

Yuan Weixing;Yuan Xiugan;Yang Chunxin;Zhao Baojun

1996, (S1): 121-124.

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CALCULATIONAL AND EXPERIMENTAL INVESTIGATION ON FLOW FIELD FOR A SUBMERGED AIR INLET
Abstract( 1268 )

Weng Peifen;Zhou Zhewei;Guo Rongwei

1996, (S1): 125-128.

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RESEARCH ON THE CURED SHAPE OF CROSS PLY UNSYMMETRIC COMPOSITE LAMINATED SHELL
Abstract( 1764 )

Ren Libo;Luo Xiaodong;Cui Degang

1996, (S1): 129-131.

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