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THE RESEARCH OF INCREASED LIFT AND REDUCED DRAG FOR WING-TIP SAILS
Chen Mingyan;Qi Mengbu
1994, (6): 641-646.
PDF [ 379 K ]( 545 ) HTML
RESEARCH ON DIGITAL ACTIVE FLUTTER SUPPRESSION
Zou Congqing;Chen Guibin
1994, (6): 647-651.
PDF [ 330 K ]( 496 ) HTML
AN EXPERIMENTAL INVESTIGATIOM OF BOUNDARY LAYERS DOWNSTREAM OF DISRETE FILM COOLING HOLES
Liao Guoqi;Jiang Tao;Xu Hongzhou;Liu Songling
1994, (6): 652-657.
PDF [ 316 K ]( 676 ) HTML
DESIGN AND VALIDATION OF SIMULATION SCREEN FOR INLET FLOW DISTORTION
Li Wenlan;Huang Zhitao;Qiao Weiyang
1994, (6): 658-664.
PDF [ 443 K ]( 592 ) HTML
INVESTIGATION OF ATOMIZERS EFFECT ON SOOT CONCENTRATION AND FLAME RADIATION IN A SMALL MODEL GAS TURBINE COMBUSTOR
Liu Gang;Li Li;Wu Shousheng
1994, (6): 665-671.
PDF [ 448 K ]( 406 ) HTML
ASEL-ANADA-BASED EXTENDABLE SOFTWARE ENGINEERING LANGUAGE
Xu Baowen;Yuan Ming;Lin Junhai;Bai Jinsong;Yang Hong
1994, (6): 672-678.
PDF [ 463 K ]( 357 ) HTML
COMPOSITE CHARACTERISTIC RESEARCH ON THREE TEMPERATURE-REGULATING MEASURES AIMED AT HUMAN BODY
Wang Jun;Yu Houman
1994, (6): 679-684.
PDF [ 397 K ]( 513 ) HTML
THE RIPPLE MODEL METHOD OF FAULT DIAGNOSIS TO HYDRAULIC PUMP
Wang Shaoping;Jiang Xun;Li Peiqiong;Wang Zhanlin
1994, (6): 685-690.
PDF [ 377 K ]( 405 ) HTML
CYCLIC DEFORMATION AND DISLOCATION OF TC11 TITANIUM ALLOY UNDER FATIGUE-CREEP INTERACTION
Zhou Yu;Pang Yunhong;Zhou Yigang
1994, (6): 691-695.
PDF [ 359 K ]( 480 ) HTML
SURFACE REACTION DURING DEGASSING OF RAPIDLY SOLIDIFIED AL-Li-Mg-Cu-Zr POWDERS
Dai Shenglong;Yu Guifu;Yan Minggao
1994, (6): 696-701.
PDF [ 374 K ]( 383 ) HTML
THE STUDY OF ENTERPRISE ADAPTING MECHANISM
Li Yue;Cheng Lianjun;Guo Weihong
1994, (6): 702-707.
PDF [ 406 K ]( 363 ) HTML
WALL INTERFERENCE CORRECTION OF HIGH LIFT TEST
Zhang Wenhua;A. Küpper
1994, (6): 708-711.
PDF [ 240 K ]( 551 ) HTML
CABIN NOISE SOURCE-PATH IDENTIFICATION FOR AD-200 ULTRALIGHT AIRCRAFT
Yin Jianping;Hu Zhangwei;Zhang Qiang
1994, (6): 712-715.
PDF [ 238 K ]( 578 ) HTML
GUIDELINES OF AIRCRAFT CABIN ENVIRONMENT ACOUSTICS DESIGN
Lei Shihao;Jiang Zimao
1994, (6): 716-719.
PDF [ 351 K ]( 1127 ) HTML
ACTIVE CONTROL OF SOUND RADIATED FROM AN AIRPLANE PANEL
Wang Chong;Sun Zhaohui;Hou Hong;Sun Jincai
1994, (6): 720-724.
PDF [ 256 K ]( 709 ) HTML
THEORETICAL STUDY ON THE BLADE-VORTEX INTERACTION NOISE OF HELICOPTER ROTOR
Qiao Weiyang;Tang Diyi;Li Wenlan
1994, (6): 725-730.
PDF [ 219 K ]( 490 ) HTML
DESIGN OF A HONEYCOMB SANDWISH STRUCTURE WITH GLASS FIBER REINFORCED PLASTICS FOR A LARGE SCALE WING PANEL
Wei Zhiyi
1994, (6): 731-734.
PDF [ 320 K ]( 588 ) HTML
THE RESEARCH ON ELECTRONIC TEMPERATURE DIFFERENCE AND FIX SENSOR
Lu Junfang;Liu Ying
1994, (6): 735-739.
PDF [ 410 K ]( 558 ) HTML
THE ELECTROMAGNETIC COMPATIBILITY AND DISTRIBUTION OF AIRCRAFT ANTENNA SYSTEM
Yao Yourui;Wang Baofa
1994, (6): 740-744.
PDF [ 276 K ]( 567 ) HTML
PHASE COMPENSATION FOR FBW SYSTEM
Shao Rongshi
1994, (6): 745-748.
PDF [ 239 K ]( 820 ) HTML
AN INVESTIGATION OF CHEMICAL SHORT CRACK CHARACTERISTICS IN GC-4 HIGH-STRENGTH STEEL
Wang Rong;Lou Minxu;Zhen Xiulin
1994, (6): 749-752.
PDF [ 343 K ]( 406 ) HTML
ANALYSIS OF ADHESIVE BONDED JOINTS WITH STIFFNESS UNBALANCED ADHERENDS
Yan Shilin;Liu Xiongya
1994, (6): 753-756.
PDF [ 198 K ]( 696 ) HTML
THICKNESS EFFECT ON FATIGUE CRACK PROPAGATION OF AI-ALLOY
Zhang Shijie;Zhu Yigang;Huang Xinyue;Liu Shaolun
1994, (6): 757-760.
PDF [ 283 K ]( 577 ) HTML
RESEARCH ON B4C-TiB2-W2B5 COMPOSITE
Tang Guohong;Chen Changqi;Zhang Xinghua
1994, (6): 761-764.
PDF [ 336 K ]( 375 ) HTML
SUPERSONIC SEPARATION FLOW ON A BODY OFREVOLUTION WITH POINT NOSE
Chen Nanqian;Su Li
1994, (6): 765-766.
PDF [ 169 K ]( 572 ) HTML
DEVELOPMENT DYNAMICAND APPLICATIONS OF MULTI-CHANNELTEST & ANALYSIS SYSTEM (DTAS)
Zhang Lingmi;Zhang Chunning
1994, (6): 767-768.
PDF [ 135 K ]( 450 ) HTML
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