导航
Archive
Current situation and development trend of multidisciplinary coupled adjoint system for aircraft
HUANG Jiangtao, LIU Gang, GAO Zhenghong, ZHOU Zhu, CHEN Zuobin, JIANG Xiong
doi: 10.7527/S1000-6893.2019.23404
2020, (5): 623404-623404.
PDF [ 13721 K ]( 2068 ) HTML
Recent progress of efficient global aerodynamic shape optimization using surrogate-based approach
HAN Zhonghua, XU Chenzhou, QIAO Jianling, LIU Fei, CHI Jiangbo, MENG Guanyu, ZHANG Keshi, SONG Wenping
doi: 10.7527/S1000-6893.2019.23344
2020, (5): 623344-623344.
PDF [ 10401 K ]( 2576 ) HTML
Research progress and application of ARI_OPT software for aerodynamic shape optimization
WEI Chuang, YANG Long, LI Chunpeng, ZHANG Tiejun
doi: 10.7527/S1000-6893.2019.23370
2020, (5): 623370-623370.
PDF [ 9357 K ]( 1072 ) HTML
Digital integrated platform for universal aircraft aerodynamic design optimization: DIPasda
SUN Junfeng, ZHOU Zhu, HUANG Yong, PANG Yufei, LU Fengshun, XU Yong
doi: 10.7527/S1000-6893.2019.23348
2020, (5): 623348-623348.
PDF [ 10658 K ]( 1005 ) HTML
An efficient adaptive global optimization method suitable for aerodynamic optimization
LI Chunna, ZHANG Yangkang
doi: 10.7527/S1000-6893.2019.23352
2020, (5): 623352-623352.
PDF [ 7065 K ]( 780 ) HTML
Optimization of aeroshape integrated design of winged re-entry vehicles
LI Zhengzhou, HE Yuanyuan, GAO Chang, ZHANG Xiaoqing, WANG Qi
doi: 10.7527/S1000-6893.2019.23356
2020, (5): 623356-623356.
PDF [ 6919 K ]( 1392 ) HTML
Three dimensional radar cross section geometric sensitivity calculation based on discrete adjoint equation
ZHOU Lin, HUANG Jiangtao, GAO Zhenghong
doi: 10.7527/S1000-6893.2019.23361
2020, (5): 623361-623361.
PDF [ 3874 K ]( 613 ) HTML
Aerodynamic design optimization of a single low-speed compressor stage by an adjoint method
LUO Jiaqi, YANG Jing
doi: 10.7527/S1000-6893.2019.23368
2020, (5): 623368-623368.
PDF [ 4104 K ]( 821 ) HTML
Aerodynamic optimization design of large civil aircraft using pressure distribution inverse design method based on discrete adjoint
LIU Fengbo, JIANG Cheng, MA Tuliang, LIANG Yihua
doi: 10.7527/S1000-6893.2019.23372
2020, (5): 623372-623372.
PDF [ 13754 K ]( 738 ) HTML
Strategies and methods for multi-objective aerodynamic optimization design for supercritical wings
LI Runze, ZHANG Yufei, CHEN Haixin
doi: 10.7527/S1000-6893.2019.23409
2020, (5): 623409-623409.
PDF [ 4658 K ]( 1198 ) HTML
Multi-objective aerodynamic optimization algorithm based on manifold reconstruction
SONG Chao, LI Weibin, ZHOU Zhu, LIU Hongyang, LAN Qingsheng
doi: 10.7527/S1000-6893.2019.23687
2020, (5): 623687-623687.
PDF [ 4538 K ]( 731 ) HTML
Research on injury and brace position for front-row occupant under horizontal impact
XIE Jiang, MA Shicheng, HE Yonglong, YANG Yongpan, FENG Zhenyu, WANG Yafeng, YANG Huan
doi: 10.7527/S1000-6893.2019.23489
2020, (5): 223489-223489.
PDF [ 12482 K ]( 520 ) HTML
Dynamic characteristic analysis for a folding fin with freeplay nonlinearities based on mode synthesis method
WANG Qiang, MA Zhisai, ZHANG Xin, LIU Yan, DING Qian
doi: 10.7527/S1000-6893.2019.23507
2020, (5): 223507-223507.
PDF [ 3763 K ]( 823 ) HTML
Eye movement and fatigue detection in visual inspection of civil aircraft composite materials
HE Qiang, TAN Deqiang, CHENG Lin
doi: 10.7527/S1000-6893.2019.23532
2020, (5): 223532-223532.
PDF [ 2728 K ]( 604 ) HTML
Revisit mechanism driven multi-UAV cooperative search planning method for moving targets
ZHANG Zhexuan, LONG Teng, XU Guangtong, WANG Yangjie
doi: 10.7527/S1000-6893.2019.23314
2020, (5): 323314-323314.
PDF [ 4853 K ]( 1193 ) HTML
Threat assessment based on multilayer and multistage skyline selection method
WANG Siyuan, WANG Gang, YUE Shaohua, SONG Yafei, LIU Jiayi
doi: 10.7527/S1000-6893.2019.23494
2020, (5): 323494-323494.
PDF [ 2703 K ]( 568 ) HTML
Landing-phase guidance of rocket using bias proportional guidance and convex optimization
AN Ze, XIONG Fenfen, LIANG Zhuonan
doi: 10.7527/S1000-6893.2019.23606
2020, (5): 323606-323606.
PDF [ 4551 K ]( 890 ) HTML
Allocation of composite mode on-orbit service resource based on improved DQN
LIU Bingyan, YE Xiongbing, ZHOU Chifei, LIU Biliu
doi: 10.7527/S1000-6893.2019.23630
2020, (5): 323630-323630.
PDF [ 1551 K ]( 568 ) HTML
Reliability analysis of aircraft power system based on Bayesian networks and common cause failures
KONG Xiangfen, WANG Jie, ZHANG Zhaomin
doi: 10.7527/S1000-6893.2019.23632
2020, (5): 323632-323632.
PDF [ 3342 K ]( 1053 ) HTML
Backstepping sliding mode control of electric dynamic load simulator based on extended state observer
DAI Mingguang, QI Rong
doi: 10.7527/S1000-6893.2020.23683
2020, (5): 323683-323683.
PDF [ 3990 K ]( 460 ) HTML
Stability of 2D pressure servo valve considering cavitation effect
LONG Qian, RUAN Jian, LI Sheng, HE Jinfei
doi: 10.7527/S1000-6893.2019.23281
2020, (5): 423281-423281.
PDF [ 5642 K ]( 436 ) HTML
Atypical failure mechanism of aero-engine main shaft roller bearing
ZHENG Jintao, DENG Sier, ZHANG Wenhu, DANG Xiaoyong
doi: 10.7527/S1000-6893.2019.23347
2020, (5): 423347-423347.
PDF [ 6423 K ]( 747 ) HTML
Static and dynamic characteristics of magnetic suspension coupling
MENG Bin, WANG Deng, XU Hao, LIU Bei
doi: 10.7527/S1000-6893.2019.23358
2020, (5): 423358-423358.
PDF [ 6385 K ]( 416 ) HTML
Stylus orientation optimization method in five-axis on-machine measurement based on feasible graph
ZHUANG Qixin, MO Rong, WAN Neng, GUO Yanheng
doi: 10.7527/S1000-6893.2019.23403
2020, (5): 423403-423403.
PDF [ 4974 K ]( 512 ) HTML
Academic Quality
Download Ranking
CJA