导航
Archive
TRANSONIC WALL INTERFERENCE CORRECTIONS FOR CIVIL AIRCRAFT MODEL TESTS
Fanzhaolin;Cui Naiming;Yun qilin;Yin Luping
1994, (2): 129-135.
PDF [ 455 K ]( 355 ) HTML
STUDY ON ROTOR HEAD ABSORBER OF HELICOPTER
Gu Zhongquan;Pen Fujun;Ma Kougen
1994, (2): 136-140.
PDF [ 413 K ]( 570 ) HTML
PERCENT REGRESSION ANALYSIS
Fu Huimin
1994, (2): 141-148.
PDF [ 420 K ]( 692 ) HTML
FAULT-TOLERANCE TYPE OF AUTOMATIC DE-ICING SYSTEM FOR AIRCRAFT
Chang Wenxiu;Tao Jianwu;Dong Qingwei
1994, (2): 149-154.
PDF [ 377 K ]( 393 ) HTML
THEN Nd-Fe-B PERMANENT MAGNET DCMICROMACHINE
Zhu Yaozhong
1994, (2): 155-160.
PDF [ 391 K ]( 406 ) HTML
THE MICROCOMPUTER CONTROL AUTOMATION FOR AIR TO AIR MISSILE TESTER
Qu Xinsheng;Wang Chenhua;Xu Xinqun;Zhang Xun;Zhang Chijun
1994, (2): 160-162.
PDF [ 273 K ]( 309 ) HTML
THE APPLICATION OF INTEGRATED SIMULATION TECHNOLOGY IN FLIGHT MANAGEMENT SYSTEM
Liu Jimei;Zheng Tanliao
1994, (2): 163-168.
PDF [ 363 K ]( 478 ) HTML
RESEARCH OF OPTICAL METHOD FOR NON-DESTRUCTIVE DETECTION ON METALLIC HIVELIKE ASSEMBLY
Lu Fuyi;Zhang Chaohui;Li Enpu;Chen Changle
1994, (2): 169-174.
PDF [ 488 K ]( 424 ) HTML
CUTTER LOCATIONS GENERATION OF 5-AXES NC MILLING FOR POCKETS BOUNDED BY SCULPTURED SURFACES
He Weiping;Zhang Dinghua
1994, (2): 175-180.
PDF [ 395 K ]( 553 ) HTML
STUDY ON MONITORING OF TOOL BREAKAGE FOR VIBRATION TAPPING IN TITANIUM ALLOYS
Zhang Deyuan;Han Yuntai;Chen Dingchang
1994, (2): 181-187.
PDF [ 442 K ]( 636 ) HTML
AN INVESTIGATION ON THE RESTRAINT OF FRICTIONAL TEMPERATURE-RISE BY ION IMPLANTATION
Wang Yihua;Hu Zhengqiong;Yin Keli
1994, (2): 188-191.
PDF [ 369 K ]( 365 ) HTML
LOW TEMPERATURE TENSILE AND NOTCHED TENSILE PROPERTIES OF A RAPIDLY SOLIDIFIED Al-Li ALLOY
Mi Xujun;Yuan Guansen;Zhao Zhuoyong
1994, (2): 192-196.
PDF [ 405 K ]( 445 ) HTML
STUDY ON FATIGUE TEST TECHNIQUE OF CONTINUOUS VARIABLE STROKE FOR AIRCRAFT LANDING GEARS
Feng Peili;Zhang Lianbn
1994, (2): 197-199.
PDF [ 278 K ]( 491 ) HTML
DYNAMIC OPTIMIZATION OF THERMAL STRUCTURE
Chen Jifeng;Duan Degao;Wang Jingen
1994, (2): 200-203.
PDF [ 223 K ]( 647 ) HTML
THE APPLICATION OF AN APPROXIMATE DECOUPLING METHOD TO THE THE FLIGHT CONTROL SYSTEMS
Zhang Weiguo;Xiao Shunda
1994, (2): 205-210.
PDF [ 327 K ]( 3203 ) HTML
THE STUDY ON COUPLING DISTURBANCE OF THE FLIGHT MECHANI-CAL CONTROL SYSTEM WITH SERVO-MECHANISM SYSTEM IN AIRCRAFT
Wang Yibing;Feng Yachang;Wang Zhan lin
1994, (2): 212-218.
PDF [ 395 K ]( 432 ) HTML
EXPERIMENTAL INVESTIGATION ON CHANGE OF COLDWODKING RESIDUAL STRAIN OF HOLE IN ALUMINIUM ALLOY SHEET
Lin ying;Wu Fumin;Xing Wenzhen
1994, (2): 219-221.
PDF [ 120 K ]( 649 ) HTML
BUCKLING OF COMPOSITE SANDWICH CONSTRUCTION UNDER TWISTING AND BENDING MOMENTS
Xu Ze;Cheng Yiebiao;Wei Zengsu
1994, (2): 222-227.
PDF [ 277 K ]( 517 ) HTML
GROWTH CALCULATION OF CIRCULAR FATIGUE CRACK ON MAIN LANDING GEAR SHOCK ABSORBING CYLINDER
Gao jinhua;Li Benxu;Liu Ruichen
1994, (2): 228-231.
PDF [ 239 K ]( 586 ) HTML
A METHOD FOR DETERMINING THE STABILITY OF MOTION
He Tianming
1994, (2): 232-235.
PDF [ 320 K ]( 419 ) HTML
DOUBLE-STRESS ACCELERATED MODELING AND PARAMETER ESTIMATION
Wang Shaoping;Li Peiqiong;Wang Zhanlin
1994, (2): 236-241.
PDF [ 335 K ]( 856 ) HTML
INVESTIGATION OF HIGH STRENGTH AND HEAT-RESISTING CAST Al-SI ALLOY
Jia Jun;Cheng Yuyong;Gui Manchang;Zhu Jian
1994, (2): 242-245.
PDF [ 214 K ]( 580 ) HTML
RESEARCHING OF SiCp
Xu Yongli;YangEnzhong;Chen Biankun
1994, (2): 246-249.
PDF [ 133 K ]( 419 ) HTML
INVESTIGATION OF THE ACCURATE CONTROL ABOUTSURFACE CARBON CONCENTRATION OF CARBURISING PART
Wu Xinwen;Xi Shoumou;Yang Shipin;Zhen Xiangmo
1994, (2): 250-253.
PDF [ 348 K ]( 443 ) HTML
Academic Quality
Download Ranking