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THE RELATIONSHIP BETWEEN THE AERODYNAMIC CHARACTERISTICS OF DOUBLE-DELTA WINGS AND VORTICES WITH SIDESHIPS AT HIGH ANGLES OF ATTACK
Bao Guohua
1988, (8): 317-323.
PDF [ 939 K ]( 347 ) HTML
OPTIMUM DESIGN OF COMPOSITE LAMINATES CONSIDERING INTERLAMINA STRESS
Yang Bingxian
1988, (8): 324-329.
PDF [ 409 K ]( 338 ) HTML
EFFECT OF BLADE MISTUNING AND BLADE-DISK ON CASCADE FLUTTER BOUNDARIES
Chen Jingbo;Chen Qun;Shen Dakuan;Fan Feida
1988, (8): 330-337.
PDF [ 521 K ]( 351 ) HTML
ALIGNMENT AND CALIBRATION OF STRAPDOWN INERTIAL NAVIGATION SYSTEM IN A SWAYING VEHICLE
Yuan Xin;Ni Yongxi
1988, (8): 338-345.
PDF [ 535 K ]( 402 ) HTML
MEASURMENTS OF THE BUFFET BOUNDARY OF WINGS IN TRANSONIC FLOW WITH HOT-FILM METHOD
Wang Qiaosen;Qiu Xuejun;Zhang Zhaoming
1988, (8): 346-351.
PDF [ 372 K ]( 296 ) HTML
MAINTENANCE REFORM FOR HOME-MADE CIVILIAN AIRCRAFT SYSTEMS AND EQUIPMENTS
Gu Chengchung;Zhong Hongchun
1988, (8): 352-358.
PDF [ 484 K ]( 338 ) HTML
THE COMBINATION OF SIMULATION AND RESPONSE SURFACE METHODOLOGY AND ITS APPLICATION IN AN AGGREGATE PRODUCTION PLAN
Chen Zhiming;Feng Yuncheng
1988, (8): 359-365.
PDF [ 495 K ]( 395 ) HTML
THEROTETICAL ANALYSIS OF "ENGINEERING EXPERIENCE METHOD
Yang Weimin;Tu Qingci;Lu Tingxiao
1988, (8): 366-374.
PDF [ 550 K ]( 412 ) HTML
AN INVESTIGATION OF WALL INTERFERENCE CORRECTION TO THE PRES SURE MEASUREMENT IN LOW SPEED WIND TUNNEL WITH SOLID WALLS
Jiang Guiqing
1988, (8): 375-380.
PDF [ 533 K ]( 401 ) HTML
SELECTION OF THE OPTIMAL LIGHTER-THAN-AIR GAS FOR AIRSHIP AND A SCHEME OF DOUBLE-LAYER STRUCTURAL DESIGN
Wang Youfu;Chang Dayong
1988, (8): 381-382.
PDF [ 154 K ]( 507 ) HTML
THE GENERAL RULE OF BIRDS' COLLIDING AGAINST AEROPLANES AND ANTICOLLISION MEASURES
Li Qiying
1988, (8): 383-386.
PDF [ 273 K ]( 351 ) HTML
A METHOD OF COMPUTER AIDED DESIGN OF STRUCTURAL TYPE——AN APPLICATION OF EXPERT SYSTEM AND FUZZY SETS THEORY
Zhang Yongshun;Wei Fajie
1988, (8): 387-391.
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APPLICATION OF CORRELATION COEFFICIENTS TO IDENTIFICAT/ON OF PARAMETERS
Wang Chao;Zhang Jinghui
1988, (8): 392-395.
PDF [ 216 K ]( 360 ) HTML
AN EFFECTIVE SOLUTION PROCEDURE OF FEM FOR MATERIAL NONLINEAR ANALYSIS——PREDICTED SECONT STIFFNESS PROCEDURE
Lu Shan
1988, (8): 396-400.
PDF [ 322 K ]( 332 ) HTML
A SIMPLIFIED CALCULATION FOR INTERNAL FLOW OF TRANSPIRATION COOLED NOSETIP
Ren Fen;Tang Jinrong
1988, (8): 401-406.
PDF [ 339 K ]( 414 ) HTML
DESIGN OF MULTI-LEVEL FLIGHT CONTROL SYSTEMS
Feng Gang
1988, (8): 407-412.
PDF [ 337 K ]( 239 ) HTML
THE OFF-BORESIGHT LAUNCH OF AIR-TO-AIR MISSILES
Zhang Zilie;Zhang An
1988, (8): 413-418.
PDF [ 372 K ]( 954 ) HTML
OIL POURING EQUATION AND ITS DISPERSING TREATMENT FOR ISOTHERMAL FORGING AT CONSTANT STRAIN RATE
Huang Xiaobao;Chen Bing;Liu Jianyu
1988, (8): 423-427.
PDF [ 309 K ]( 219 ) HTML
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