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25 September 1983, Volume 4 Issue 3

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25 September 1983, Volume 4 Issue 3

论文

NUMERICAL SOLUTION OF HYPERSONIC FLOW NEAR LEADING EDGE OF FLAT PLATE
Abstract( 1183 )

Fu Dexun

1983, (3): 1-8.

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A NEW METHOD FOR CALCULATING SUPERSONIC UNSTEADY AERODYNAMIC FORCES AND ITS APPLICATION
Abstract( 1637 )

Wang Xianxin

1983, (3): 9-18.

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RELIABILITY ANALYSIS FOR PAIRED MAIN WING COMPONENTS
Abstract( 1368 )

Lin Fujia;Huang Yushan

1983, (3): 19-27.

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NONDESTRUCTIVE EXPERIMENTAL METHOD FOR DETERMINING CRITICAL LOADS OF SHELL STRUCTURES UNDER EXTERNAL PRESSURE
Abstract( 1525 )

Chen Huanxing;Li Wuquan;Rong Hongqun;Song Mu

1983, (3): 28-35.

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ANALYTICAL AND SEMI-ANALYTICAL METHODS FOR DYNAMIC COMPUTATIONS OF LAMINATED PLATES MADE OF FIBRE-REINFORCED OR HOMOGENEOUS LAYERS
Abstract( 1203 )

Cao Zhiyuan;Zhang Yaoqin

1983, (3): 36-46.

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INVESTIGATION ON TWO-DIMENSIONAL AIRBLAST ATOMIZER
Abstract( 1514 )

Zhao Qishott;Yin Xingliang;Hou Muyu

1983, (3): 47-55.

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EFFECT OF A SHEAR LAYER ON STABILITY OF AN AXISYMMETRIC EXTERNAL COMPRESSION AIR INTAKE
Abstract( 1446 )

Zhang Kunyuan;Yu Shaozhi;Peng Chenyi

1983, (3): 56-62.

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A TERRAIN-AIDED NAVIGATION SYSTEM
Abstract( 1850 )

Chen Huihuang

1983, (3): 63-75.

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CALCULATION FOR ATTITUDE ANGLES OF AN ALL ATTITUDE AEROPLANE STRAPDOWN SYSTEM
Abstract( 2046 )

Chen Zhe

1983, (3): 76-85.

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A NEW METHOD FOR CALCULATING STRAPDOWN DIRECTION COSINE MATRIX
Abstract( 2130 )

Liu Hengchun

1983, (3): 86-93.

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MINIMUM WEIGHT DESIGN OF DISKS
Abstract( 1299 )

Ren Jilin

1983, (3): 94-101.

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COMMENT ON "DETERMINATION OF AERODYNAMIC COEFFICIENTS FOR A REENTRY BODY BY MEANS OF AN EXTENDED KALMAN FILTER
Abstract( 1630 )

Cai Jinshi

1983, (3): 102-103.

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