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THE AERODYNAMIC BEHAVIOURS Or VORTICES FOR SLENDER-WING
Deng Xueying
1989, (8): 351-359.
PDF [ 673 K ]( 309 ) HTML
THE ANALYSIS AND SOLUTION OF THE PERFORMANCE DETERIORATION PROBLEM OF WP7 ENGINE UNDER THE FULL REHEATING CONDITION
Shang Yi;Wang Yanzhong;Wu Zizhong
1989, (8): 360-365.
PDF [ 420 K ]( 471 ) HTML
THE OPTIMAL DESIGN OF MULTIPASS ELECTRIC -HYDRAULIC SERVO SYSTEMS WITH FORCE BALANCE TYPE
Wang Zhanlin;Shi Li
1989, (8): 366-372.
PDF [ 338 K ]( 275 ) HTML
A DISCRETE-TIME MODEL REFERENCE ADAPTIVE CONTROLLER IN THE PRESENCE OF UNCERTAIN DISTURBANCES
Bao Pingan;Zhou Fengqi
1989, (8): 373-380.
PDF [ 442 K ]( 402 ) HTML
THE OPTIMUM CONTROL AND ADAPTIVE CONTROL FOR AIRPLANE CABIN PRESSURE
Ying Wenjiang
1989, (8): 381-388.
PDF [ 424 K ]( 247 ) HTML
SIMULATION FOR AXI SYMMETRIC FORWARD EXTRUSION BY RIGID-PLASTIC FINITE ELEMENT METHOD
Wu Shichun;Cheng Xiuquan
1989, (8): 389-396.
PDF [ 587 K ]( 313 ) HTML
APPLICATIONS OF DAMAGE MECHANICS IN THE PROBLEMS OF HIGH CYCLE FATIGUE OF METALS
Ruan Xiaoping;Zhang Xing
1989, (8): 397-402.
PDF [ 337 K ]( 264 ) HTML
A METHOD OF MODIFICATION TO ALLOW FOR THE EDGE-EFFECT OF THE LAMINATE OF FINITE WIDTH ON THE TENSILE STRENGTH
Li Shunlin;Xiao Jun
1989, (8): 403-408.
PDF [ 419 K ]( 304 ) HTML
A NEW METHOD FOR CONSTRUCTING DIGITAL-STRAIN -FIELD-IMAGE FROM MOIRE PATTERN
Yu Qifeng;Long Dibo
1989, (8): 409-412.
PDF [ 515 K ]( 291 ) HTML
STUDY OF DRILLING (EXPANDING) TECHNOLOGY ON PMMA USED IN AIRPLANE CANOPY
Wang Ziming
1989, (8): 413-418.
PDF [ 753 K ]( 347 ) HTML
THE APPLICATION AND DESIGN OF LARGE INTEGRAL PANELS FOR SH-5 AIRCRAFT
Lan Zhifang
1989, (8): 419-424.
PDF [ 384 K ]( 312 ) HTML
APPLICATIONS OF PHASE DATA IN FAULT DIAGNOSIS
Yue Guojin;Wang Keming;Yan Litang;Li Qihan
1989, (8): 425-431.
PDF [ 500 K ]( 462 ) HTML
THE INDUCED VELOCITY DISTRIBUTION AND THE FLAP- PITCH-TORSION COUPLING ON THE STABILITY AND CONTROL OF THE HELICOPTER IN FLIGHT CONDITION WITH LATERAL VELOCITY
Cao Yihua;Xu Xinyu
1989, (8): 432-438.
PDF [ 374 K ]( 309 ) HTML
ON THE RELATIONSHIP BETWEEN YIELD STRESS AND FATIGUE CRACK INITIATION LIFE OF METALS
Zheng Xiulin
1989, (8): 439-442.
PDF [ 265 K ]( 420 ) HTML
BASIC PRINCIPLES OF MEASURING THRUST THROUGH EXHAUST TO INLET TOTAL PRESSURE RAT10-ENGINE PRESSURE RATIO EPR
Cui Jiya
1989, (8): 443-446.
PDF [ 235 K ]( 601 ) HTML
EXPERIMENTAL INVESTIGATION ON FLOW CHARACTERISTICS OF THE RECIRCULATION ZONE BEHIND VEE-GUTTER FLAMEHOLDER
Li Gaiqi;Wang Jiahua
1989, (8): 447-449.
PDF [ 169 K ]( 438 ) HTML
THE STUDY ON A FIRE CONTROL PRINCI PLE OF AIR- TO-AIR MISSLE FOR TARGET OFF-BORESIGHT LAUNCH IN AII-ROUND ATTACK
Gao Xiaoguang;Zhang Zilie
1989, (8): 450-454.
PDF [ 321 K ]( 452 ) HTML
AN INVESTIGATION OF BIMETALLIC-DISK THERMOSTATS BY MEANS OF FINITE ELEMENT SIMULATION
Ren Xiaoan
1989, (8): 455-458.
PDF [ 403 K ]( 288 ) HTML
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