THE INFLUENCES OF FORCED OSCILLATIONS TOWARD VORTEX-BREAKDOWN
Chen Yan-qiu;Lu Zhi-yong and Lee Chun-hianBeijing University of Aeronautics and Astronautics

..............page:327-332

A COMPLETE BOUNDARY INTEGRAL FORMULATION FOR STEADY COMPRESSIBLE INVISCID FLOWS GOVERNED BY NONLINEAR EQUATIONS
Yang Zuo-sheng Nanjing Aeronautical Institute

..............page:333-338

A CALCULATING METHOD OF THE KILL PROBABILITY ATTACK AREA FOR AAM
Li Ting-jie;Liu Run-quan and Wang Chao-zhiBeijing University of Aeronautics and Astronautics Zhu Gu-xiang and Wang Li-zhen014 Center of Ministry of Aeronautics and Astronautics

..............page:339-346

THE MODAL FEATURES OF THE VIBRATION SYSTEMS OF THE WEAKLY- VISCOELASTIC MATERIAL STRUCTURES
Chen Guo-ping and Zhu De-maoNanjing Aeronautical Institute

..............page:347-353

A STUDY ON MECHANICAL MODEL OF THE HELICOPTER "GROUND RESONANCE
Gu Zhong-quan Nanjing Aeronautical Institute

..............page:354-360

TRANSONIC FLOW CALCULATION OF EULER EQUATIONS BY IMPLICIT ITERATING SCHEME WITH FLUX SPLITTING
Liu Dao-zhi and Zha Ge-chengBeijing University of Aeronautics and Astronautics

..............page:361-368

NUMERICAL INVESTIGATION OF AXIAL FLOW COMPRESSOR CASING TREATMENT
Zhuang PingInstitute of Engineering Thermo physics Lu Ya-jun and Cui Ji-ya Beijing University of Aeronautics & Astronautics

..............page:369-379

GROWTH BEHAVIOR OF SHORT FATIGUE CRACKS FOR ALUMINUM- LITHIUM ALLOY 8090
Chen Zheng Northwestern Polytechnical University

..............page:380-385

A DISCUSSION ON THE RELATIONSHIP BETWEEN THE IMPACT TOUGHNESS AND THE FRACTURE TOUGHNESS
Xu Chang-gan Beijing University of Aeronautics and Astronautics Yu Gang Helsinki University of Technology;Finland

..............page:386-392