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Development of future fighters
YANG Wei
doi: 10.7527/S1000-6893.2020.24377
2020, (6): 524377-524377.
PDF [ 4047 K ]( 15450 ) HTML
Key technologies and future applications of thrust vectoring on fighter aircraft
WANG Haifeng
doi: 10.7527/S1000-6893.2020.24057
2020, (6): 524057-524057.
PDF [ 11144 K ]( 5725 ) HTML
Review of aeroelasticity design for advanced fighter
LI Qiuyan, LI Gang, WEI Yangtian, RAN Yuguo, WU Bo, TAN Guanghui, LI Yan, CHEN Shi, LEI Boqi, XU Qinwei
doi: 10.7527/S1000-6893.2019.23430
2020, (6): 523430-523430.
PDF [ 10636 K ]( 2794 ) HTML
Review of numerical research on unsteady flows of the new generation fighters
XIAO Zhixiang, CUI Wenyao, LIU Jian, LUO Kunyu, SUN Yuanhao
doi: 10.7527/S1000-6893.2019.23451
2020, (6): 523451-523451.
PDF [ 13827 K ]( 1608 ) HTML
Review of aircraft battle damage assessment and repair estimation and design technology
ZU Guangran, PEI Yang, HOU Peng
doi: 10.7527/S1000-6893.2019.23455
2020, (6): 523455-523455.
PDF [ 5134 K ]( 1635 ) HTML
Development and application of strength design technology of high performance fighter
ZHANG Lixin, ZHONG Shunlu, LIU Xiaodong, FU Huanbing, DUI Hongna, LIU Dongliang, JING Luyun, MOU Binjie, SHI Shanglu
doi: 10.7527/S1000-6893.2019.23480
2020, (6): 523480-523480.
PDF [ 13824 K ]( 1708 ) HTML
Application of integrated thermal management in development of advanced fighter system
TU Min, YUAN Gengmin, XUE Fei, WANG Xiaoming
doi: 10.7527/S1000-6893.2019.23629
2020, (6): 523629-523629.
PDF [ 4431 K ]( 2212 ) HTML
Recent development of safety and reliability analysis technology for model-based complex system
HU Xiaoyi, WANG Ruping, WANG Xin, FU Yongtao
doi: 10.7527/S1000-6893.2019.23436
2020, (6): 523436-523436.
PDF [ 5530 K ]( 2835 ) HTML
Prediction and assessment of drop separation compatibility of internal weapons by wind tunnel drop-test
SONG Wei, AI Bangcheng, JIANG Zenghui, LU Wei
doi: 10.7527/S1000-6893.2019.23415
2020, (6): 523415-523415.
PDF [ 9344 K ]( 982 ) HTML
Comprehensive study on yaw control characteristic of combined control surfaces of flying wing configuration
ZHOU Zhu, YU Yonggang, LIU Gang, CHEN Zuobin, HE Kaifeng
doi: 10.7527/S1000-6893.2019.23422
2020, (6): 523422-523422.
PDF [ 12279 K ]( 1303 ) HTML
Gravity effects of light model method in wind tunnel model drop-test
DONG Jingang, XIE Feng, ZHANG Chenkai, MA Handong, QIN Yongming
doi: 10.7527/S1000-6893.2019.23434
2020, (6): 523434-523434.
PDF [ 4473 K ]( 622 ) HTML
Unsteady aerodynamic modeling for fighter configuration at high angles of attack
SHEN Lin, HUANG Da, WU Genxing, ZHAN Jingxia
doi: 10.7527/S1000-6893.2019.23440
2020, (6): 523440-523440.
PDF [ 9012 K ]( 1351 ) HTML
Wind tunnel model flight test technique for advanced fighter aircraft design
CEN Fei, NIE Bowen, LIU Zhitao, GUO Linliang, SUN Haisheng, LI Qing
doi: 10.7527/S1000-6893.2019.23444
2020, (6): 523444-523444.
PDF [ 4739 K ]( 1213 ) HTML
After body supersonic directional stability augmentation method for tailless configuration
LI Chunpeng, LIU Tiezhong, QIAN Zhansen, ZHANG Tiejun
doi: 10.7527/S1000-6893.2019.23447
2020, (6): 523447-523447.
PDF [ 8264 K ]( 1228 ) HTML
Air data fusion and estimation method for advanced aircrafts in post-stall maneuver
YANG Zhaoxu, GUO Yi, LEI Tingwan, LI Rongbing
doi: 10.7527/S1000-6893.2019.23456
2020, (6): 523456-523456.
PDF [ 4662 K ]( 997 ) HTML
Inlet aerodynamic characteristics of fighter under high angle of attack and post-stall maneuver
XIANG Huan, YANG Yingkai, XIE Jinrui, WU Yongsheng
doi: 10.7527/S1000-6893.2019.23460
2020, (6): 523460-523460.
PDF [ 4952 K ]( 1040 ) HTML
Life support system in advanced fighter
BAO Xiaoning, ZHAO Peilin, ZHANG Baozhong, HU Zhiwen, LAN Yuqing, XUE Fei
doi: 10.7527/S1000-6893.2019.23464
2020, (6): 523464-523464.
PDF [ 7285 K ]( 1513 ) HTML
Radar cross-section effect of canard
GUO Zhanzhi, CHEN Yingwen, MA Lianfeng
doi: 10.7527/S1000-6893.2019.23485
2020, (6): 523485-523485.
PDF [ 4964 K ]( 2737 ) HTML
Time delay stability boundary on relaxed static stability aircraft
CHEN Xiaoming, SUN Shaoshan, TAO Chenggang, TANG Yong
doi: 10.7527/S1000-6893.2019.23487
2020, (6): 523487-523487.
PDF [ 3742 K ]( 691 ) HTML
Design and regulation of aircraft maintainability based on technique model
LYU Gangde, WANG Haifeng, DENG Wei
doi: 10.7527/S1000-6893.2019.23453
2020, (6): 523453-523453.
PDF [ 2961 K ]( 587 ) HTML
Military airplane health assessment technique based on data mining of flight parameters
FANG Guancheng, JIA Dapeng, LIU Yifei, LIU Haitao
doi: 10.7527/S1000-6893.2019.23458
2020, (6): 523458-523458.
PDF [ 3528 K ]( 1203 ) HTML
Key technologies and design of new generation fighter canopy
YANG Bo, ZHAO Peilin, CAI Sanjun, ZHOU Shenglin, CHEN Chuan
doi: 10.7527/S1000-6893.2019.23465
2020, (6): 523465-523465.
PDF [ 6214 K ]( 1408 ) HTML
Strength desigh and test of advanced fighter all-moving twin V-tail buffet
JIN Wei, YANG Zhichun, MENG Dehong, CHEN Yan, HUANG Hu, WANG Yongjun, HE Shi, CHEN Yuanfang
doi: 10.7527/S1000-6893.2019.23473
2020, (6): 523473-523473.
PDF [ 9508 K ]( 1322 ) HTML
Engineering design and analysis technique of aeroelastic characteristics of composite wing
YANG Jun, CHANG Nan, GAN Xuedong, GAN Jian, LIU Jian
doi: 10.7527/S1000-6893.2019.23477
2020, (6): 523477-523477.
PDF [ 3167 K ]( 983 ) HTML
Full-scale aircraft strength test technology of next generation fighter
WANG Yupeng, PEI Lianjie, LI Qiulong, ZHENG Jianjun, FENG Jianmin, WANG Fan
doi: 10.7527/S1000-6893.2019.23482
2020, (6): 523482-523482.
PDF [ 5651 K ]( 1716 ) HTML
Dynamic reconfiguration method based on effectiveness for advanced fighter avionics system
ZHAO Changxiao, HE Feng, LI Hao, WANG Peng
doi: 10.7527/S1000-6893.2019.23416
2020, (6): 523416-523416.
PDF [ 3507 K ]( 828 ) HTML
Intelligent virtual training partner in embedded training system of fighter
CHEN Bin, WANG Jiang, WANG Yang
doi: 10.7527/S1000-6893.2019.23467
2020, (6): 523467-523467.
PDF [ 8895 K ]( 1261 ) HTML
Development and application of large-scale damage tolerance titanium alloy TC4-DT
CHEN Lianguo, WANG Wensheng, ZHU Zhishou, ZHAO Yong, HUANG Jianyun, ZHANG Hai, PENG Fuhua
doi: 10.7527/S1000-6893.2019.23454
2020, (6): 523454-523454.
PDF [ 4949 K ]( 1136 ) HTML
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