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Calibration method for constant temperature hot-wire anemometer for compressible fluid
DU Yufeng, LIN Jun, MA Husheng, LIANG Jinmin
doi: 10.7527/S1000-6893.2016.0283
2017, (6): 120600-120600.
PDF [ 4104 K ]( 672 ) HTML
Design and performance analysis of practical curved cone waverider inlet
HE Xuzhao, LE Jialing
doi: 10.7527/S1000-6893.2016.0289
2017, (6): 120690-120690.
PDF [ 11908 K ]( 1044 ) HTML
New method for predicting 3-D water droplet impingement on rotor considering influence of shadow zone
CHEN Xi, ZHAO Qijun
doi: 10.7527/S1000-6893.2016.0313
2017, (6): 120745-120745.
PDF [ 14845 K ]( 711 ) HTML
Test on effects of porous permeable section on trailing edge noise
LIU Hanru, CHEN Nanshu
doi: 10.7527/S1000-6893.2016.120746
2017, (6): 120746-120746.
PDF [ 13246 K ]( 599 ) HTML
Numerical simulation of effect of steady blowing slot-less flap airfoil in ground effect
JIANG Yubiao, WANG Wanbo, CHANG Zhiqiang, HUANG Yong
doi: 10.7527/S1000-6893.2016.120751
2017, (6): 120751-120751.
PDF [ 12404 K ]( 658 ) HTML
Computation analyses of aeroelastic loads of rotor based on CFD/CSD coupling method
MA Li, ZHAO Qijun, ZHAO Mengmeng, WANG Bo
doi: 10.7527/S1000-6893.2016.0292
2017, (6): 120762-120762.
PDF [ 8205 K ]( 1294 ) HTML
Similarity rule and Mach number scaling law for simplified landing gear noise
XING Yu, LIU Peiqing, GUO Hao, XU Liang, LI Ling
doi: 10.7527/S1000-6893.2016.0290
2017, (6): 120769-120769.
PDF [ 4968 K ]( 615 ) HTML
Junction flow horseshoe vortex control based on upstream cavity
LI Jian, ZHANG Hua, WU Xinggang
doi: 10.7527/S1000-6893.2016.0304
2017, (6): 120796-120796.
PDF [ 23530 K ]( 483 ) HTML
Dynamic stall suppression for rotor airfoil based on inflatable leading edge technology
XU Heyong, XING Shilong, YE Zhengyin, MA Mingsheng
doi: 10.7527/S1000-6893.2016.0308
2017, (6): 120799-120799.
PDF [ 12648 K ]( 833 ) HTML
Design and property advantages analysis of double swept waverider
LIU Chuanzhen, BAI Peng, CHEN Bingyan
doi: 10.7527/S1000-6893.2016.0291
2017, (6): 120808-120808.
PDF [ 8482 K ]( 810 ) HTML
Aerodynamic design of low-Reynolds-number wing taking into account the multiple propellers induced effects
WANG Kelei, ZHOU Zhou, ZHU Xiaoping
doi: 10.7527/S1000-6893.2016.120813
2017, (6): 120813-120813.
PDF [ 8434 K ]( 804 ) HTML
An optimization method for dynamic identification based on short-duration maneuvering flight test data
WANG Baoyin, ZHANG Shuguang, JIA Xiaopeng
doi: 10.7527/S1000-6893.2016.0293
2017, (6): 120815-120815.
PDF [ 4079 K ]( 540 ) HTML
Vibration response of sandwich panels with gradient metallic cellular core
XIAO Dengbao, ZHAO Guiping
doi: 10.7527/S1000-6893.2016.220576
2017, (6): 220576-220576.
PDF [ 5293 K ]( 373 ) HTML
Precision analysis of deployable structures based on dimension reduction method and effective link length
QI Junwei, WANG Chunjie, DING Jianzhong
doi: 10.7527/S1000-6893.2016.0273
2017, (6): 220590-220590.
PDF [ 2665 K ]( 727 ) HTML
Method for evaluating powered high-lift effects of externally blown flap
ZHANG Shengwei, WANG Wei
doi: 10.7527/S1000-6893.2016.0272
2017, (6): 220689-220689.
PDF [ 2939 K ]( 637 ) HTML
Crashworthiness of composite corrugated beam based on nonlinear progressive damage model
JIANG Hongyong, REN Yiru, YUAN Xiuliang, GAO Binhua
doi: 10.7527/S1000-6893.2016.220717
2017, (6): 220717-220717.
PDF [ 25360 K ]( 930 ) HTML
Unsteady aerodynamic reduced-order modeling method for parameter changeable structure
WANG Ziyi, ZHANG Weiwei
doi: 10.7527/S1000-6893.2017.120829
2017, (6): 220829-220829.
PDF [ 4084 K ]( 554 ) HTML
Influence of platform swaying on accuracy of Kalman filter tracking
CHENG Han, CHEN Weiyi, XIE Zhiliang
doi: 10.7527/S1000-6893.2016.0249
2017, (6): 320589-320589.
PDF [ 3277 K ]( 509 ) HTML
PD-type learning observer based fault reconstruction for spacecraft attitude control systems
ZHANG Ke, HAN Zhiguo, GUO Xiaohong, LYU Meibo
doi: 10.7527/S1000-6893.2016.0259
2017, (6): 320629-320629.
PDF [ 2784 K ]( 471 ) HTML
Energy-optimal in orbit mission planning for agile remote sensing satellites
ZHAO Lin, WANG Shuo, HAO Yong, LIU Yuan
doi: 10.7527/S1000-6893.2016.0298
2017, (6): 320654-320654.
PDF [ 6326 K ]( 3752 ) HTML
Broadband signal DOA estimation based on sparse representation and l0-norm approximation
YAN Xuezhi, WEN Yanxin, LIU Guohong, CHEN Jian
doi: 10.7527/S1000-6893.2016.320705
2017, (6): 320705-320705.
PDF [ 2598 K ]( 460 ) HTML
A robust beamformer with a polarization sensitive array and polarization estimation
YU Xiang, LI Dan, ZHANG Jianqiu
doi: 10.7527/S1000-6893.2016.0312
2017, (6): 320752-320752.
PDF [ 2643 K ]( 396 ) HTML
Design of moving-mass attitude control system for nanosatellites in orbital transfer stage
LU Zhengliang, ZHANG Xiang, YU Yongjun, MO Qiankun, LIAO Wenhe
doi: 10.7527/S1000-6893.2016.0306
2017, (6): 320778-320778.
PDF [ 4341 K ]( 520 ) HTML
A user defined method for machining features in NC programming of complex structural parts
LIU Changqing, LI Yingguang, WANG Pengcheng, HAO Xiaozhong
doi: 10.7527/S1000-6893.2016.420735
2017, (6): 420735-420735.
PDF [ 15928 K ]( 566 ) HTML
Assembly variation optimization method of aircraft compliant parts based on active locating compensation of fixture
ZHANG Wei, WANG Zhiguo, TAN Changbai, LIU Xia
doi: 10.7527/S1000-6893.2016.420862
2017, (6): 420862-420862.
PDF [ 4534 K ]( 489 ) HTML
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