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25 August 1992, Volume 13 Issue 8

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25 August 1992, Volume 13 Issue 8

论文

ON THE MODIFICATION OF THE CORRECTION RULE FOR SIDEWALL INTERFERENCE IN TWO-DIMENSIONAL WIND TUNNELS
Abstract( 1480 )

Cheng Ke-ming

1992, (8): 353-356.

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OPTIMUM DESIGN CALCULATION OF MULTIELEMENT AIRFOILS
Abstract( 1998 )

Lu Zhi-liang;Ren Ji-ye;Tao Di

1992, (8): 357-361.

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FLUTTER WHIRL OF THE PROPELLER ROTOR SYSTEMS
Abstract( 1251 )

Gu Jia-liu;Hong Jie;Li Shang-fu

1992, (8): 362-369.

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INVESTIGATION ON THE MECHANISM OF EXTENDING STABILITY FOR HUB TREATMENT
Abstract( 1346 )

Du Zhao-hui;Liu zhi-wei

1992, (8): 370-373.

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VECTOR ANALYSIS METHOD FOR PROPELLER BALANCING
Abstract( 2130 )

Fu Xi-shou

1992, (8): 374-381.

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DISTRIBUTED AVIONICS SOFTWARE TEST SYSTEM
Abstract( 1757 )

Zhu Yi-an;Kang Ji-chang;Han Zhao-xuan

1992, (8): 382-386.

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A STUDY OF HIERARCHICAL AVIONIC INTEGRATED SIMULATION SYSTEM
Abstract( 1873 )

Li Wei-hua;Kang Ji-chang;Han Zhao-xuan;Zhou Xing-she

1992, (8): 387-392.

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THE USE OF ORDER LANGUAGES IN THE DIGITAL FLIGHT CONTROL SYSTEMS
Abstract( 1326 )

Yang Yi-dong

1992, (8): 393-400.

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THE CHARACTERISTICS OF AERODYNAMIC FORCE ON CREWMAN ARMS DURING WINDBLAST
Abstract( 1627 )

Teng Yu-ying;You Guang-xing;Zhang Shu-he;Zhuang Xiang-chang

1992, (8): 401-406.

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CROSS-TALK ELIMINATION OF MULTICOMPONENT FORCE SENSOR
Abstract( 1428 )

Jin Wen-lin Zhang You-zhen

1992, (8): 407-411.

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STUDY ON METHANE-CONTROLLED CARBON-POTENTIAL
Abstract( 1204 )

Wu Suo-chun;Feng Jian-xun

1992, (8): 412-417.

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METHOD OF THE COMBINATION OF VARYING-LIP AND PLATE SIMULATING TOTAL PRESSURE DISTORTED FLOW FIELD
Abstract( 2047 )

Chen Xiao;Mao Jian

1992, (8): 418-422.

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SELECTION OF COMPRESSION RATIOS IN DESIGN OF OLEO-PNEUMATIC SHOCK-STRUT OF LANDING GEAR
Abstract( 1290 )

Nie Hong;Qiao Xin

1992, (8): 423-426.

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DYNAMIC RESPONSE OF THE AILERON BALANCE WEIGHT DURING LANDING IMPACT
Abstract( 1891 )

Huang Shu-chun;Wang Chang-yuan

1992, (8): 427-430.

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A DYNAMIC MODEL OF MECHANISM AND CALCULATION IN PLANE MOTION
Abstract( 1201 )

Li Su

1992, (8): 431-433.

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HUMAN RELIABILITY ANALYSIS IN AUTOMATIC AVIATION SYSTEMS
Abstract( 1888 )

Dai Guang-ya

1992, (8): 434-438.

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RESEARCH ON AIRCRAFT SUPPORTABILITY
Abstract( 2066 )

Wang Li-qun

1992, (8): 439-443.

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THERMO-PEHL ANALYSIS FOR THE SURFACE FLASH TEMPERATURE OF POWER TRANSMISSION GEARS
Abstract( 1301 )

Chen Guo-ding;Li Dong-zi

1992, (8): 444-447.

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DYNAMIC RESPONSE ANALYSIS OF COMPOSITE STRUCTURE DURING LAUNCHING MISSILE
Abstract( 2265 )

He Lian-zhu;Zhao Pei-ling

1992, (8): 448-451.

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GENERAL FRAMEWORK OF PLANNING MANAGEMENT AND DECISION-MAKING SYSTEM FOR DEVELOPMENT OF NEW AIRCRAFT
Abstract( 2235 )

Ning Xuan-xi;Zhang Ke-min

1992, (8): 452-455.

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INVESTIGATION OF NEAR-THRESHOLD FATIGUE CRACK PROPAGATION BEHAVIOUR IN 300M ULTRA-HIGH STRENGTH STEEL
Abstract( 2605 )

Ding Chuan-fu

1992, (8): 456-460.

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THE CALCULATION OF DYNAMIC DERIVATIVES OF WINGS IN HYPERSONIC FLOW
Abstract( 1760 )

Chen Jin-song

1992, (8): 461-462.

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