1000-6893
2016 Issue 8
..............page:封3
PREFACE
chen jian qiang ;
chen jian qiang ;
..............page:前插1
..............page:前插2
A review of unsteady aerodynamic modeling of aircrafts at high angles of attack
WANG Qing;,QIAN Weiqi;,DING Di;
WANG Qing;,QIAN Weiqi;,DING Di;
..............page:2331-2347
Research progress of numerical method of dynamic stability derivatives of aircraft
LIU Xu;,LIU Wei;,CHAI Zhenxia;,YANG Xiaoliang;
LIU Xu;,LIU Wei;,CHAI Zhenxia;,YANG Xiaoliang;
..............page:2348-2369
Research status of aircraft interior noise
ZUO Kongcheng;,CHEN Peng;,WANG Zheng;,TIAN Hao;,TANG Daofeng;
ZUO Kongcheng;,CHEN Peng;,WANG Zheng;,TIAN Hao;,TANG Daofeng;
..............page:2370-2384
Problems in numerical prediction of dynamic stability derivatives
YUAN Xianxu;,CHEN Qi;,XIE Yufei;,CHEN Jianqiang;
YUAN Xianxu;,CHEN Qi;,XIE Yufei;,CHEN Jianqiang;
..............page:2385-2394
Unstructured deforming mesh and discrete geometric conservation law
LIU Jun;,LIU Yu;,CHEN Zedong;
LIU Jun;,LIU Yu;,CHEN Zedong;
..............page:2395-2407
A new method of wall profile design for shape-controllable shock wave enhancement
ZHAN Dongwen;,YANG Jianting;,YANG Jiming;,ZHU Yujian;
ZHAN Dongwen;,YANG Jianting;,YANG Jiming;,ZHU Yujian;
..............page:2408-2416
Double degree-of-freedom large amplitude oscillation test technology in low speed wind tunnel
LIU Chunming;,ZHAO Zhijun;,BU Chen;,WANG Jianfeng;,MU Weiqiang;
LIU Chunming;,ZHAO Zhijun;,BU Chen;,WANG Jianfeng;,MU Weiqiang;
..............page:2417-2425
A model attitude control and measurement technique for improving quality of wind tunnel dynamic test data
LIU Zhitao;,SUN Haisheng;
LIU Zhitao;,SUN Haisheng;
..............page:2426-2435
Temperature effects on noise in subsonic swirling jets
YANG Haihua;,ZHOU Lin;,WAN Zhenhua;,SUN Dejun;
YANG Haihua;,ZHOU Lin;,WAN Zhenhua;,SUN Dejun;
..............page:2436-2444
Large eddy simulation for forced transition flow at hypersonic inlet
ZHAO Xiaohui;,DENG Xiaobing;,MAO Meiliang;,YANG Wei;,ZHAO Huiyong;
ZHAO Xiaohui;,DENG Xiaobing;,MAO Meiliang;,YANG Wei;,ZHAO Huiyong;
..............page:2445-2453
Roughness element induced hypersonic boundary layer transition
DUAN Zhiwei;,XIAO Zhixiang;
DUAN Zhiwei;,XIAO Zhixiang;
..............page:2454-2463
Unsteady aerodynamic modeling and identification for a complicated aircraft configurations
YANG Wen;,BU Chen;,SUI Jianjun;,SHANG Zuming;
YANG Wen;,BU Chen;,SUI Jianjun;,SHANG Zuming;
..............page:2464-2471
Numerical simulation of fluctuating pressure of fighter vertical tail
MENG Dehong;,SUN Yan;,WANG Yuntao;,LI Wei;
MENG Dehong;,SUN Yan;,WANG Yuntao;,LI Wei;
..............page:2472-2480
Numerical simulation investigation of aerodynamic interference of sting support in wind tunnel test of a delta wing at big angles of attack
ZHANG Jun;,AI Yu;,HUANG Da;,LIU Jing;
ZHANG Jun;,AI Yu;,HUANG Da;,LIU Jing;
..............page:2481-2489
A method for effectiveness analysis of flow separation control by local actuation based on Lagrangian coherent structures
KANG Wei;,ZHANG Quanqi;,DAI Xiangyan;,LIU Lei;
KANG Wei;,ZHANG Quanqi;,DAI Xiangyan;,LIU Lei;
..............page:2490-2497
Interactive aerodynamic characteristics of canard rotor wing aircraft in helicopter forward flight
SUN Wei;,GAO Zhenghong;,JIANG Jiechu;
SUN Wei;,GAO Zhenghong;,JIANG Jiechu;
..............page:2498-2506
Research and application of coupled simulation techniques of PID controller and CFD
CHEN Qi;,GUO Yongyan;,XIE Yufei;,CHEN Jianqiang;,YUAN Xianxu;
CHEN Qi;,GUO Yongyan;,XIE Yufei;,CHEN Jianqiang;,YUAN Xianxu;
..............page:2507-2516
Roll instability and control during pitching maneuver for a missile with strake wings
WANG Xiaobing;,ZHAO Zhongliang;,LI Hao;,DA Xingya;,TAO Yang;
WANG Xiaobing;,ZHAO Zhongliang;,LI Hao;,DA Xingya;,TAO Yang;
..............page:2517-2524
Analysis of flying vehicle's dynamic characteristics based on numerical virtual flight technology
HUANG Yu;,YAN Chao;,XI Ke;,WANG Wen;
HUANG Yu;,YAN Chao;,XI Ke;,WANG Wen;
..............page:2525-2538
Simulation of helicopter rotor in ground effect based on CFD method and hybrid trim algorithm
ZHU Mingyong;,ZHAO Qijun;,WANG Bo;
ZHU Mingyong;,ZHAO Qijun;,WANG Bo;
..............page:2539-2551
Numerical simulations for unsteady vortex flowfield of rotors based on high-order WENO scheme
YIN Zhizhao;,ZHAO Qijun;,WANG Bo;
YIN Zhizhao;,ZHAO Qijun;,WANG Bo;
..............page:2552-2564
Numerical simulation of rolling characteristics in nose-up process of square cross section vehicle
CHEN Jianqiang;,CHEN Qi;,YUAN Xianxu;,XIE Yufei;
CHEN Jianqiang;,CHEN Qi;,YUAN Xianxu;,XIE Yufei;
..............page:2565-2573
Influence of a 3/4 open jet floor on far field noise measurements in aeroacoustic wind tunnel
ZHANG Jun;,CHEN Peng;,LEI Hongsheng;,ZHANG Junlong;,LI Zhengchu;
ZHANG Jun;,CHEN Peng;,LEI Hongsheng;,ZHANG Junlong;,LI Zhengchu;
..............page:2574-2582
Analysis of dynamic characteristics between prototype aircraft and scaled-model of virtual flight test in wind tunnel
GUO Linliang;,ZHU Minghong;,KONG Peng;,NIE Bowen;,ZHONG Chengwen;
GUO Linliang;,ZHU Minghong;,KONG Peng;,NIE Bowen;,ZHONG Chengwen;
..............page:2583-2593
Analysis of dynamic performance and test data precision of models with high angle of attack
li qi chang ;, zhao zhong liang ;, yang hai yong ;, ma shang ;, li yu ping ;, liu wei liang ;, shi xiao jun ;, wang xiao bing ;
li qi chang ;, zhao zhong liang ;, yang hai yong ;, ma shang ;, li yu ping ;, liu wei liang ;, shi xiao jun ;, wang xiao bing ;
..............page:2594-2602
Test of high lift system flow control by plasma aerodynamic actuation
LIANG Hua;,WU Yun;,LI Jun;,HAN Menghu;,MA Jie;
LIANG Hua;,WU Yun;,LI Jun;,HAN Menghu;,MA Jie;
..............page:2603-2613
Test of unsteady flow in the tip clearance of low speed axial flow compressor
GAO Limin;,LI Yongzeng;,LIU Xiaodong;,ZHANG Shuai;
GAO Limin;,LI Yongzeng;,LIU Xiaodong;,ZHANG Shuai;
..............page:2614-2622