导航
Archive
Research progress and prospect for conceptual and aerodynamic technology of blended-wing-body civil aircraft
WANG Gang, ZHANG Binqian, ZHANG Minghui, SANG Weimin, YUAN Changsheng, LI Dong
doi: 10.7527/S1000-6893.2019.23046
2019, (9): 623046-623046.
PDF [ 16067 K ]( 1323 ) HTML
Review of non-circular cross-section fuselage structure design research on blended-wing-body civil aircraft
ZHANG Yongjie, WU Yingying, ZHAO Shuwang, SI Jiangtao, YUAN Changsheng
doi: 10.7527/S1000-6893.2019.23054
2019, (9): 623054-623054.
PDF [ 17362 K ]( 812 ) HTML
Analysis and optimization of overall parameters for blended-wing-body civil aircraft
CHAI Xiao, CHEN Yingchun, TAN Zhaoguang, CHEN Zhenli, SI Jiangtao, LI Jie, ZHANG Binqian
doi: 10.7527/S1000-6893.2019.23042
2019, (9): 623042-623042.
PDF [ 6353 K ]( 570 ) HTML
Cabin layout design for BWB civil aircraft based on airworthiness compliance
PAN Lijun, WU Dawei, TAN Zhaoguang, ZHANG Yizhe, CHAI Xiao, YUAN Changsheng, CHEN Yingchun
doi: 10.7527/S1000-6893.2019.23044
2019, (9): 623044-623044.
PDF [ 7939 K ]( 616 ) HTML
High-lift technology for spoiler on blended-wing-body civil aircraft
WANG Gang, ZHANG Minghui, MAO Jun, SANG Weimin, CHEN Zhenli, WANG Long, ZHANG Binqian
doi: 10.7527/S1000-6893.2019.23045
2019, (9): 623045-623045.
PDF [ 14637 K ]( 550 ) HTML
Design of Krueger flap for civil aircraft with blended-wing-body
ZHANG Minghui, CHEN Zhenli, MAO Jun, WANG Gang, TAN Zhaoguang, WANG Long, ZHANG Binqian
doi: 10.7527/S1000-6893.2019.23048
2019, (9): 623048-623048.
PDF [ 12482 K ]( 596 ) HTML
Powered-on nacelle design on blended-wing-body configuration with podded engines
GU Wenting, ZHAO Zhenshan, ZHOU Hanwei, FENG Jian, TAN Zhaoguang, LI Dong
doi: 10.7527/S1000-6893.2019.23047
2019, (9): 623047-623047.
PDF [ 13340 K ]( 467 ) HTML
Design of slat of blended-wing-body low speed testing aircraft
ZHONG Yuan, CHEN Yong, CHEN Zhenli, TAN Zhaoguang, WU Dawei, SI Jiangtao
doi: 10.7527/S1000-6893.2019.23050
2019, (9): 623050-623050.
PDF [ 7136 K ]( 341 ) HTML
Blended-wing-body aircraft overhanging engine layout technology based on numerical simulation
ZHAO Zhenshan, FENG Jian, MIAO Shuming, DU Yu
doi: 10.7527/S1000-6893.2019.23051
2019, (9): 623051-623051.
PDF [ 6804 K ]( 255 ) HTML
Tradeoff design of high and low speed performance for blended-wing-body civil aircraft
ZHANG Minghui, CHEN Zhenli, GU Wenting, LI Dong, ZHANG Shuai, YUAN Changsheng, WANG Long, ZHANG Binqian
doi: 10.7527/S1000-6893.2019.23052
2019, (9): 623052-623052.
PDF [ 7480 K ]( 422 ) HTML
Fuselage-engine aerodynamic interference effects of blended-wing-body aircraft
ZHOU Hanwei, CHEN Yong, TAN Zhaoguang, SI Jiangtao, LI Jie, LI Dong
doi: 10.7527/S1000-6893.2019.23063
2019, (9): 623063-623063.
PDF [ 6217 K ]( 506 ) HTML
Buckling and progressive damage analysis of representative compressed PRSEUS panel in blended-wing-body civil aircraft
ZHANG Yongjie, WU Yingying, ZHU Shengli, WANG Bintuan, TAN Zhaoguang, YUAN Changsheng
doi: 10.7527/S1000-6893.2019.23185
2019, (9): 623185-623185.
PDF [ 16545 K ]( 428 ) HTML
A review of three neural network methods for manufacturing feature recognition
SHI Yenan, ZHENG Guolei
doi: 10.7527/S1000-6893.2019.22840
2019, (9): 22840-022840.
PDF [ 7355 K ]( 332 ) HTML
Vibration characteristics analysis of pressurized repair hydraulic pipe of civil aircraft based on ANSYS Workbench
JIA Baohui, YU Lingjie, LU Xiang
doi: 10.7527/S1000-6893.2019.22828
2019, (9): 222828-222828.
PDF [ 5361 K ]( 218 ) HTML
Energy-absorbing characteristics of a typical sub-cargo fuselage section of a transport category aircraft
FENG Zhenyu, CHENG Kun, ZHAO Yifan, LI Henghui, XIE Jiang, MOU Haolei, WANG Yafeng, Ge Yujing
doi: 10.7527/S1000-6893.2019.22907
2019, (9): 222907-222907.
PDF [ 10268 K ]( 365 ) HTML
Vibration energy transmission characteristics of casing based on structural intensity method
MA Yingqun, XU Meng, ZHANG Kai, ZHAO Wei, ZHAO Qingjun
doi: 10.7527/S1000-6893.2019.22938
2019, (9): 222938-222938.
PDF [ 24788 K ]( 180 ) HTML
Fitting algorithm of ground-to-air missile launching area based on deep learning
GAO Xiaoguang, LI Xinyu, YUE Mengqi, ZHANG Jinhui, ZHAO Liqiang, WU Gaofeng, LI Fei
doi: 10.7527/S1000-6893.2019.22858
2019, (9): 322858-322858.
PDF [ 6610 K ]( 314 ) HTML
Spectrum sharing method for dual satellite in space information network
WANG Chuang, HU Jing, LI Yongqiang, BIAN Dongming, LI Song
doi: 10.7527/S1000-6893.2019.22863
2019, (9): 322863-322863.
PDF [ 6026 K ]( 193 ) HTML
A TDOA/FDOA passive location algorithm with the minimum number of stations
SUN Ting, DONG Chunxi, DONG Yangyang, LIU Mingming
doi: 10.7527/S1000-6893.2019.22902
2019, (9): 322902-322902.
PDF [ 4695 K ]( 438 ) HTML
Hierarchical planning for on-orbit self-reconfiguration of modular reconfigurable satellites
WANG Bo, YE Dong, SUN Zhaowei, TANG Shengyong, CHEN Xin
doi: 10.7527/S1000-6893.2019.22912
2019, (9): 322912-322912.
PDF [ 6980 K ]( 341 ) HTML
3-D simulation of internal dielectric charging characteristics of spacecraft dielectric disc structure
YUAN Qingyun, WANG Song, HUANG Xinxin
doi: 10.7527/S1000-6893.2019.23035
2019, (9): 323035-323035.
PDF [ 5537 K ]( 125 ) HTML
A testability index allocation method based on quadratic allocation
YANG Peng, XIE Haoyu, QIU Jing
doi: 10.7527/S1000-6893.2019.23070
2019, (9): 323070-323070.
PDF [ 4112 K ]( 248 ) HTML
Foundation and assessment of testability growth model considering testability design limitation rectifying delay function
LI Tianmei, SI Xiaosheng, YANG Zonghao, XU Congqi, ZHANG Qi
doi: 10.7527/S1000-6893.2019.23079
2019, (9): 323079-323079.
PDF [ 3698 K ]( 149 ) HTML
Power domain non-orthogonal pulse modulation based on prolate spheroidal wave function
LU Faping, WANG Hongxing, LIU Chuanhui, CHEN Zhaonan, KANG Jiafang
doi: 10.7527/S1000-6893.2019.23102
2019, (9): 323102-323102.
PDF [ 5355 K ]( 167 ) HTML
Force analysis and layout of cutter assemblies in robotic automatic tool changing system
JIANG Junxia, ZHU Wenjie, ZHU Weidong
doi: 10.7527/S1000-6893.2019.22824
2019, (9): 422824-422824.
PDF [ 8737 K ]( 249 ) HTML
Vibration attenuation for finishing assembly interfaces of vertical tail section of large aircraft based on novel eddy current damper
FAN Wei, ZHENG Lianyu, ZHAO Xiong, YANG Yiqing, LIU Xinyu, YANG Sen
doi: 10.7527/S1000-6893.2019.22859
2019, (9): 422859-422859.
PDF [ 16204 K ]( 164 ) HTML
Academic Quality
Download Ranking