Review on large-scale cryogenic wind tunnel and key technologies
Liao Daxiong;Huang Zhilong;Cheng Zhenhua;Tang Gengsheng;State Key Laboratory of Aerodynamics;China Aerodynamics Research and Development Center;

..............page:1-6+20

Experimental studyof shock interactingwith well-controlled gas cylinder generated bysoapfilm
Luo Xisheng;Wang Xiansheng;Chen Mojun;Zhai Zhigang;Advanced Propulsion Laboratory;Department of Modern Mechanics;University of Science and Technology of China;

..............page:7-13+26

Experimental and calculational study on convective heat transfer of n-decane under supercritical pressure
Zhang Lei;Zhang Ruoling;Xiao Shide;Zhang Xiangwen;Le Jialing;School of Mechanical Engineering;Southwest Jiaotong University;Science and Technology Laboratory on Scramjet;China Aerodynamics Research and Development Center;School of Chemical Engineering;Tianjin University;

..............page:14-20

Study on flight test of vertical-fin buffeting response of aircraft
Li Xiaolu;Tang Kai;Lei Ming;Chinese Flight Test Establishment;

..............page:21-26

Research on the experimental technology of plasma active flow control in high speed wind tunnel
Li Feng;Gao Chao;Zheng Borui;Wang Yushuai;National Key Laboratory of Aerodynamic Design and Research;Northwestern Polytechnical University;

..............page:27-31+44

The measurement of weak current velocity on water surface under wind wave environment based on linear array CCD
Liu Li;Wang Xiaoqing;Chen Pengzhen;Chong Jinsong;National Key Laboratory of Science and Technology on Microwave Imaging;Institute of Electronics;Chinese Academy of Sciences;University of Chinese Academy of Sciences;

..............page:32-38

Temperature correction of flexible thermal shear stress sensor for underwater measurements
Ma Binghe;Wang Yi;Jiang Chengyu;Li Yanbing;Wang Leitao;Key Lab of Micro/Nano Systems for Aerospace;Ministry of Education;Northwestern Polytechnical University;

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

Comparative study between PIV and three-hole wake probe measurements in the compressor plane cascade flow field
Ma Changyou;Hou Minjie;Ling Daijun;Xing Xiaolong;China Gas Turbine Establishment;Aviation Industry Corporation of China;

..............page:45-50+58

The development of a transonic wet steam wind tunnel with tunable Mach number
Li Shizhu;Cai Xiaoshu;Yu Jianfeng;Li Dianxi;Gao Yang;Li Junfeng;He Naibo;University of Shanghai for Science and Technology;703Research Institute of China Shipbuilding Industry Corporation;

..............page:51-58

Aerodynamic and structural design of large recirculating boundary-layer wind tunnel
Yu Shice;Jiang Jianqun;Lou Wenjuan;Sun Bingnan;College of Civil Engineering and Architecture;Zhejiang University;

..............page:59-64+68

Experimental research on supersonic impinging jet by rainbow schlieren
Wu Wentang;Hong Yanji;Ye Jifei;Jiang Guanlei;State Key Laboratory of Laser Propulsion and Application;Academy of Equipment;Beijing Institute of Tracking and Communication;

..............page:65-68

Auto-ignition investigation with low-pressure argon stream for arc heated wind tunnel
Zhu Chao;Yao Feng;Chen Dejiang;Zhou Wei;Li Zeyu;Hypervelocity Aerodynamics Institute of China Aerodynamics Research and Development Center;

..............page:69-72

Recent progress on spacecraft breakup model
Lan Shengwei;Liu Sen;Li Yi;Huang Jie;China Aerodynamics Research and Development Center;

..............page:73-78+104

Research on hypervelocity impact characteristics of concrete building structures target
Niu Wenxia;Huang Jie;Ke Fawei;Liang Shichang;Jian Hexiang;Liu Sen;China Aerodynamics Research and Development Center;

..............page:79-84

Numerical simulation study on tungsten rod oblique penetrating aluminum plate with attack angle
Chen Hong;Zhou Zhixuan;Huang Jie;China Aerodynamics Research and Development Center;

..............page:85-89

Study on radiation characteristics of ricochet debris cloud from aluminum plate subjected to hypervelocity impacts by aluminum projectile
Ma Zhaoxia;Huang Jie;Shi Anhua;Su Tie;Liu Sen;China Aerodynamics Research and Development Center;

..............page:90-94

Upgrading of 200 meter free-flight ballistic range at CARDC
Jiao Dezhi;Huang Jie;Ping Xinhong;Xie Aimin;Luo Jinyang;Liu Sen;China Aerodynamics Research and Development Center;

..............page:95-98

Test and simulation of N-shape shield configuration
Wen Xuezhong;Ke Fawei;Chen Ping;Ma Zhaoxia;Huang Jie;China Aerodynamics Research and Development Center;

..............page:99-104