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A review of unsteady aerodynamic modeling of aircrafts at high angles of attack
WANG Qing, QIAN Weiqi, DING Di
doi: 10.7527/S1000-6893.2016.0072
2016, (8): 2331-2347.
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Research progress of numerical method of dynamic stability derivatives of aircraft
LIU Xu, LIU Wei, CHAI Zhenxia, YANG Xiaoliang
doi: 10.7527/S1000-6893.2016.0098
2016, (8): 2348-2369.
PDF [ 8310 K ]( 1198 ) HTML
Research status of aircraft interior noise
ZUO Kongcheng, CHEN Peng, WANG Zheng, TIAN Hao, TANG Daofeng
doi: 10.7527/S1000-6893.2016.0073
2016, (8): 2370-2384.
PDF [ 9939 K ]( 1094 ) HTML
Problems in numerical prediction of dynamic stability derivatives
YUAN Xianxu, CHEN Qi, XIE Yufei, CHEN Jianqiang
doi: 10.7527/S1000-6893.2016.0180
2016, (8): 2385-2394.
PDF [ 10110 K ]( 1350 ) HTML
Unstructured deforming mesh and discrete geometric conservation law
LIU Jun, LIU Yu, CHEN Zedong
doi: 10.7527/S1000-6893.2016.0141
2016, (8): 2395-2407.
PDF [ 5837 K ]( 573 ) HTML
A new method of wall profile design for shape-controllable shock wave enhancement
ZHAN Dongwen, YANG Jianting, YANG Jiming, ZHU Yujian
doi: 10.7527/S1000-6893.2016.0071
2016, (8): 2408-2416.
PDF [ 7962 K ]( 464 ) HTML
Double degree-of-freedom large amplitude oscillation test technology in low speed wind tunnel
LIU Chunming, ZHAO Zhijun, BU Chen, WANG Jianfeng, MU Weiqiang
doi: 10.7527/S1000-6893.2016.0154
2016, (8): 2417-2425.
PDF [ 8173 K ]( 454 ) HTML
A model attitude control and measurement technique for improving quality of wind tunnel dynamic test data
LIU Zhitao, SUN Haisheng
doi: 10.7527/S1000-6893.2016.0155
2016, (8): 2426-2435.
PDF [ 11730 K ]( 595 ) HTML
Temperature effects on noise in subsonic swirling jets
YANG Haihua, ZHOU Lin, WAN Zhenhua, SUN Dejun
doi: 10.7527/S1000-6893.2016.0100
2016, (8): 2436-2444.
PDF [ 9460 K ]( 800 ) HTML
Large eddy simulation for forced transition flow at hypersonic inlet
ZHAO Xiaohui, DENG Xiaobing, MAO Meiliang, YANG Wei, ZHAO Huiyong
doi: 10.7527/S1000-6893.2016.0200
2016, (8): 2445-2453.
PDF [ 8566 K ]( 743 ) HTML
Roughness element induced hypersonic boundary layer transition
DUAN Zhiwei, XIAO Zhixiang
doi: 10.7527/S1000-6893.2016.0130
2016, (8): 2454-2463.
PDF [ 9322 K ]( 632 ) HTML
Unsteady aerodynamic modeling and identification for a complicated aircraft configurations
YANG Wen, BU Chen, SUI Jianjun, SHANG Zuming
doi: 10.7527/S1000-6893.2016.0094
2016, (8): 2464-2471.
PDF [ 4626 K ]( 541 ) HTML
Numerical simulation of fluctuating pressure of fighter vertical tail
MENG Dehong, SUN Yan, WANG Yuntao, LI Wei
doi: 10.7527/S1000-6893.2016.0121
2016, (8): 2472-2480.
PDF [ 9363 K ]( 666 ) HTML
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
doi: 10.7527/S1000-6893.2016.0095
2016, (8): 2481-2489.
PDF [ 6793 K ]( 509 ) HTML
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
doi: 10.7527/S1000-6893.2015.0363
2016, (8): 2490-2497.
PDF [ 8047 K ]( 593 ) HTML
Interactive aerodynamic characteristics of canard rotor wing aircraft in helicopter forward flight
SUN Wei, GAO Zhenghong, JIANG Jiechu
doi: 10.7527/S1000-6893.2016.0092
2016, (8): 2498-2506.
PDF [ 10935 K ]( 1510 ) HTML
Research and application of coupled simulation techniques of PID controller and CFD
CHEN Qi, GUO Yongyan, XIE Yufei, CHEN Jianqiang, YUAN Xianxu
doi: 10.7527/S1000-6893.2016.0093
2016, (8): 2507-2516.
PDF [ 10935 K ]( 749 ) HTML
Roll instability and control during pitching maneuver for a missile with strake wings
WANG Xiaobing, ZHAO Zhongliang, LI Hao, DA Xingya, TAO Yang
doi: 10.7527/S1000-6893.2016.0101
2016, (8): 2517-2524.
PDF [ 5852 K ]( 686 ) HTML
Analysis of flying vehicle's dynamic characteristics based on numerical virtual flight technology
HUANG Yu, YAN Chao, XI Ke, WANG Wen
doi: 10.7527/S1000-6893.2016.0120
2016, (8): 2525-2538.
PDF [ 6032 K ]( 684 ) HTML
Simulation of helicopter rotor in ground effect based on CFD method and hybrid trim algorithm
ZHU Mingyong, ZHAO Qijun, WANG Bo
doi: 10.7527/S1000-6893.2015.0335
2016, (8): 2539-2551.
PDF [ 18096 K ]( 548 ) HTML
Numerical simulations for unsteady vortex flowfield of rotors based on high-order WENO scheme
YIN Zhizhao, ZHAO Qijun, WANG Bo
doi: 10.7527/S1000-6893.2015.0281
2016, (8): 2552-2564.
PDF [ 11390 K ]( 671 ) HTML
Numerical simulation of rolling characteristics in nose-up process of square cross section vehicle
CHEN Jianqiang, CHEN Qi, YUAN Xianxu, XIE Yufei
doi: 10.7527/S1000-6893.2016.0150
2016, (8): 2565-2573.
PDF [ 9315 K ]( 508 ) HTML
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
doi: 10.7527/S1000-6893.2016.0184
2016, (8): 2574-2582.
PDF [ 3755 K ]( 433 ) HTML
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
doi: 10.7527/S1000-6893.2015.0296
2016, (8): 2583-2593.
PDF [ 4028 K ]( 721 ) HTML
Analysis of dynamic performance and test data precision of models with high angle of attack
LI Qichang, ZHAO Zhongliang, YANG Haiyong, MA Shang, LI Yuping, LIU Weiliang, SHI Xiaojun, WANG Xiaobing
doi: 10.7527/S1000-6893.2016.0123
2016, (8): 2594-2602.
PDF [ 5892 K ]( 529 ) HTML
Test of high lift system flow control by plasma aerodynamic actuation
LIANG Hua, WU Yun, LI Jun, HAN Menghu, MA Jie
doi: 10.7527/S1000-6893.2016.0131
2016, (8): 2603-2613.
PDF [ 6952 K ]( 542 ) HTML
Test of unsteady flow in the tip clearance of low speed axial flow compressor
GAO Limin, LI Yongzeng, LIU Xiaodong, ZHANG Shuai
doi: 10.7527/S1000-6893.2016.0099
2016, (8): 2614-2622.
PDF [ 7410 K ]( 547 ) HTML
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