MEASUREMENT　OF　THE　COAXIALROTOR　FLOWFIELDIN　HOVERING　USING　3D　LASER　DOPPLER　VELOCIMETER
Tang　Zhengfei Li　Feng Gao　Zheng Mei　WeishengInstitute　of　the　Helicopter　Technology;Nanjing　University　of　Aeronautics　and　Astronautics;Nanjing 210016

..............page:82-88

INFRARED　IMAGING　TECHNIQUE　FOR　SURFACE　FLOW　VISUALIZATION
Tian　Yupeng Wang　Tiecheng Zhao　ZhongfuDept.of　Aero.Nanjing　University　of　Aeronautics　and　Astronautics;Nanjing 210016

..............page:89-92

SHOCK　MOTION　AND　WALL　PRESSURE　FLUCTUATION　INA　HYPERSONIC　TURBULENT　SEPARATED　FLOW
Wang Shifen Ren ZhiyuanInstitute of Mechanics;Chinese Academy of Sciences;Beijing 100080

..............page:75-81

EXPERIMENTAL　STUDY　ON　THE　PHENOMENON　OFTWOPHASE　EXPLOSION　IN　A　LARGE　SCALE　TUBE
Chen　Zhihua Fan　Baochun Liu　Qingming Li　HongzhiNanjing　University　of　Science　&　Technology;Nanjing 210094

..............page:45-50,63

HIGH　ANGLE　OF　ATTACK　DYNAMIC　DERIVATIVEEXPERIMENT　TECHNIQUE　IN1.2M　WIND　TUNNEL
Zhao Zhongliang Ren BinChina Aerodynamics Research & Development Center;Mianyang 621000

..............page:57-63

HIGH　ENTHALPY　EQUILIBRIUM　FLOW　ANDMEASUREMENTS　OF　STAGNATION　POINT　CONVECTIVEAND　RADIATIVE　HEAT　TRANSFER　IN　A　SHOCK　TUNNEL
Tang　Guiming Yuan　Shengxue Zeng　YuanjinInstitude　of　Mechanics;Chinese　Academy　of　Science;Beijin 100080

..............page:51-56

SYUDY　ON　THE　PROPAGATIONOF　SHOCK　WAVE　OVERSHARPEDGED　SPLITPLATE
Le　Jialing Cheng　YangshengChina　Aerodynamics　Research　&　DevelopmentCenter;Mianyang　621000

..............page:30-38

SOME　PROBLEMS　IN　THE　EXPERIMENTALTECHNIQUES　OF　UNSTEADY　AERODYNAMICS
Lian　QixiangInst.of　Fluid　Mech;Beijing　University　of　Aeronautics　and　Astronautics;Beijing　100083

..............page:2-8

RECENT　DEVELOPMENT　IN　THE　STUDY　OF　TRANSITION　AND　TURBULENCE
Lee　CunbiaoInstitute　of　Atmospheric　Physics;Chinese　Academy　of　Sciences;Beijing 100029State　Key　Laboratory　of　Turbulence　Research　of　Beijing　University;Beijing 100871

..............page:9-29

STUDY　ON　SHOCKWAVE　DEFLECTION　ANDREFLECTION　AT　CHANNEL　PORTAL
Zhou　Liduan Gong　Wenhai Yang　Zhiguo Jin　HengzhangLuoyang　Hydraulic　Engineering　Research　Institute;Luoyang 471023

..............page:64-68

INVESTIGATION　OF　AERODYNAMIC　CHARACTERISTICSON　AN　OSCILLATING　DELTA　WING　IN　LOWSPEED
Hong　Jinsen;Fu　Guangming;Wang　QiangBeijing　Institute　of　Aerodynamic;Beijing　100074

..............page:39-44

A　FULLY　AUTOMATIC　WIND　TUNNELBALANCES　CALIBRATION　SYSTEM
Wang　ChaoanShenyang　Aerodynamic　Research　Institute;Shenyang 110034

..............page:93-97

AERODYNAMIC　DESIGN　AND　WIND　TUNNEL　TESTOF　A　TYPE　TJ-1　SUPERSONIC　SAMPLER
Yang Jichun Li WiliangNorthwest Institute of Nuclear Technology;Xian 710024

..............page:69-74