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25 February 1992, Volume 13 Issue 2

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25 February 1992, Volume 13 Issue 2

SEPARATED VORTEX SIMULATION OF WINGED VEHICLE AT HIGH ANGLES OF ATTACK
Abstract( 1453 )

Lin Bing-qiu

1992, (2): 1-6.

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DESIGN PROBLEMS OF THREE-DIMENSIONAL CONTRACTIONS
Abstract( 1604 )

Su Yao-xi;Lin Chao-qiang;Hong Liu

1992, (2): 7-13.

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BOUNDARY ELEMENT LOCAL METHOD FOR ANALYSING AND CALCL-LAT1NG AERODYNAMIC COEFFICIENTS OF ORBITER
Abstract( 1268 )

Lu Gan-yu;Shen Qing

1992, (2): 14-19.

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SOLUTION OF STRESS INTENSITY FACTORS AT CRACKS IN SHEETS AND STRINGERS OF STIFFENED PANELS
Abstract( 1282 )

Huang Weiyang

1992, (2): 20-25.

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THE ANALYSIS OF THE PROCESSING INCREASED WEIGHT FOR PILOT PRODUCTION OF F-X AIRCRAFT
Abstract( 1162 )

Liu Meng-zhao;Pan Rue-gang

1992, (2): 26-31.

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AN ANALYSIS OF DYNAMIC BEHAVIOUR OF HELICAL GEAR TRANSMISSIONS
Abstract( 1418 )

Fang Zong de;Shen Yun-wen;Gao Xiang-qun

1992, (2): 32-39.

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THE APPLICATIONS OF GLOBAL ASYMPTOTIC REACHING OF SLIDING MODE APPROACH TO CONTROL
Abstract( 1258 )

Er Lian-jie;Dai Shu-ling

1992, (2): 40-45.

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CURRENT STATUS FOR RADAR TARGET RECOGNITION TECHNIQUE
Abstract( 3049 )

Wang Bei-De

1992, (2): 46-52.

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EFFECT OF THE TURBULENCE ON BOUNDARY LAYER TRANSITION MEASUREMENT
Abstract( 1343 )

Zheng Guo-feng

1992, (2): 53-56.

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DIVERGENT AND CONVERGENT CHARACTERS OF SIMPLE METHOD
Abstract( 1540 )

Cai Da-ying;Zhang Chi-ping

1992, (2): 57-59.

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THE AIR-TO-AIR MISSILE'S ATTACKER REGION AND CAPTURE RE- GION
Abstract( 2102 )

Xiao Bao-sheng

1992, (2): 60-64.

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THE EFFECTS OF LOW-LEVEL WINDSHEAR ON AUTOMATIC LANDING OF LARGE TRANSPORT
Abstract( 1307 )

Bai Zhao-gui

1992, (2): 65-69.

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DIAGNOSIS PROGRAM OF ASCERTAINING AIRCRAFT MACHINE GUN FAILURE BY MEANS OF MINIMOM CUT-SET EFFECTIVE COEFFICIENT
Abstract( 1261 )

Xiong Yu-xi;Li Lin

1992, (2): 70-73.

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A METHOD AND A SOFTWARE FOR CONSTRUCTING FLIGHT-BY-FLIGHT RANDOM LOAD SPECTRUM
Abstract( 1565 )

Li Jan;Chen Zhi-wei

1992, (2): 74-77.

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RESEARCH ON NEAR-THRESHOLD CRACK PROPAGATION AND THRESHOLD OF CORNER-CRACK AT THE HOLE
Abstract( 1849 )

Luo Yi;Liu Wen-ting

1992, (2): 78-82.

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THEORETICAL EXPLANATION ON THE SPRAY CHARACTERISTICS UNDER HIGH BACK PRESSURES
Abstract( 1188 )

Jin Ru-shan;He Lin

1992, (2): 83-88.

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THE EXPERIMENTAL INVESTIGATION OF THE INLET DISTORTION SIMULATION EQUIPMENT
Abstract( 1170 )

Lin Qi-xun;Chen Fu-qun;Zhang Dong;Fang Xin;Gao Zhong-bo;Xian Ning-fang

1992, (2): 89-93.

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DYNAMIC PERFORMANCE OF THE ANNULAR HEAT EXCHANGER
Abstract( 1184 )

Tian Ting-chen;Shou Rong-zhong;He Hui-shan

1992, (2): 94-97.

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A COMPUTER SIMULATION TO THE DYNAMIC RESPONSES OF A HYDRO-PNEUMATIC SHOCK ABSORBER
Abstract( 1880 )

Li Xi-wen

1992, (2): 98-102.

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LONGITUDINAL CLOSED-LOOP PILOT VEHICLE ANALYSIS OF DFBW AIRCRAFT DURING APPROACH AND LANDING
Abstract( 1851 )

Feng Ya-chang;Wang Yong;Wang Zhan-lin

1992, (2): 103-106.

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THE DEVELOPMENT OF INTERACTIVE GRAPHIC PROGRAMMING SYSTEM OF NC FOR COMPLEX SURFACES
Abstract( 1395 )

Zhou Ming;Wang Shu-chun

1992, (2): 107-109.

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TECHNOLOGY FOR FINE MACHINING OF BIG DEEP BLIND HOLE IN TITANIUM ALLOYS
Abstract( 1284 )

Jiang Cheng-yu;Sun Ru-gang;Chen Hong;Mei Sheng-min

1992, (2): 110-111.

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