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作品数:773被引量:1133H指数:13
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相关作者:刘乐承刘星麟廖文和王冠军安永泉更多>>
相关机构:东南大学中北大学南京航空航天大学中国科学院更多>>
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相关基金:国家自然科学基金国家重点基础研究发展计划中国博士后科学基金国家高技术研究发展计划更多>>
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Molding simulation of airfoil foam sandwich structure and interference optimization of foam-core
《Chinese Journal of Aeronautics》2024年第10期325-338,共14页Qianying CEN Zeyang XING Qingyou WANG Lili LI Zhigang WANG Zhanjun WU Ling LIU 
Supported by the Harbin Aviation Industry Group Co.,Ltd and the National Natural Science Foundation of China(No.11972256).
During the Co-Cure Molding(CCM)of airfoil foam sandwich structure,it is challenging to avoid collapse of foam core at the trailing edge.Herein,an Equal Proportional Thickening(EPT)method is proposed to optimize the in...
关键词:Airfoil foam sandwich structure Polymethacrylimide(PMI)foam INTERFERENCE CO-CURING Molding simulation 
Influence of bolt dynamic installation on topography characteristics and mechanical behaviors of CFRP interference-fit bolted joints
《Chinese Journal of Aeronautics》2024年第2期482-500,共19页Xiaohe WANG Zengqiang CAO Yuehaoxuan WANG Yingjiang GUO 
co-supported by the National Commercial Aircraft Manufacturing Engineering Innovation Fund,China(No.COMAC-SFGS-2-22-1816);Shaanxi Province Key Research and Development Program Projects,China(No.2022GXLH-02025);Shaanxi Province 100 Scientific and Technological Achievements Transformation Action Projects,China(No.2021CGBX-11)。
As the controlled research of Dynamic Installation(DI)and Static Installation(SI),a new interference installation method was developed based on electromagnetic loading to enhance the mechanical properties of composite...
关键词:Carbon Fiber-Reinforced Polymer(CFRP) Bolted joints Interference-fit Electromagnetic installation Finite Element Analysis(FEA) Damage mechanics Bearing behavior 
Interference and grinding characteristics in ultra-precision grinding of thin-walled complex structural component using a ball-end grinding wheel被引量:2
《Chinese Journal of Aeronautics》2021年第4期192-207,共16页Tingzhang WANG Henan LIU Chunya WU Jian CHEN Mingjun CHEN 
the National Key Research and Development Program of China(No.2018YFB 1107600)。
As for ultra-precision grinding of difficult-to-process thin-walled complex components with ball-end grinding wheels,interference is easy to occur.According to screw theory and grinding kinematics,a mathematical model...
关键词:Ultra-precision grinding Complex component Ball-end grinding wheel INTERFERENCE Grinding characteristics 
State estimate for stochastic systems with dual unknown interference inputs被引量:1
《Chinese Journal of Aeronautics》2020年第9期2395-2407,共13页Xiaoxue FENG Shuhui LI Feng PAN 
supported by the National Natural Science Foundation of China(Nos.61603040 and 61433003);Yunnan Applied Basic Research Project of China(No.201701CF00037);Guangdong Province Science and Technology Innovation Strategy Special Fund Project,China(No.skjtdzxrwqd2018001);Yunnan Provincial Science and Technology Department Key Research Program(Engineering),China(No.2018BA070)。
Stochastic system state estimation subject to the unknown interference input widely exists in many fields,such as the control,communication,signal processing,and fault diagnosis.However,the research results are mostly...
关键词:Adaptive filter Decoupling filter State estimate Stochastic system Unknown interference input 
Electromagnetic riveting technique and its applications被引量:28
《Chinese Journal of Aeronautics》2020年第1期5-15,共11页Zengqiang CAO Yangjie ZUO 
funded by the Major National Research Project of Numerical Control Machine and Basic Manufacturing Equipment of China(No.2016ZX04002004-008).
With the increasing applications of novel materials and structures in new-generation aircraft,conventional joining techniques in aircraft component assembly are greatly challenged.To meet those challenges,the electrom...
关键词:Composite ELECTROMAGNETIC RIVETING HOLE strengthening INTERFERENCE FIT TITANIUM alloys 
Nacelle-airframe integration design method for blended-wing-body transport with podded engines
《Chinese Journal of Aeronautics》2019年第8期1860-1868,共9页Zhenqing XIN Zhenli CHEN Wenting GU Gang WANG Zhaoguang TAN Dong LI Binqian ZHANG 
supported by the Fundamental Research Funds for the Central Universities (Nos. 3102019JC009 and G2016KY0002)
Strong shock waves and flow separation often occur during the integration of nacelle and airframe for blended-wing-bodies with podded engines. To address this problem, this paper presents an integration method with nu...
关键词:Blended-wing-body COMPUTATIONAL FLUID dynamics Drag reduction Flow INTERFERENCE Nacelle-airframe INTEGRATION 
Interference torque of a three-floated gyroscope with gas-lubricated bearings subject to a sudden change of the specific force被引量:7
《Chinese Journal of Aeronautics》2019年第3期737-747,共11页Yan LI Fuhai DUAN 
supported by the Aeronautical Science Foundation of China(No.20150863003)
A numerical study is carried out to investigate the influence of a sudden change of the specific force on a three-floated gyroscope with a rotor supported on gas-lubricated bearings.The interference torque is calculat...
关键词:Conical bearing Gas lubricated bearings INTERFERENCE TORQUE ROTOR-BEARING system Three-floated GYROSCOPE 
Computational study of wing deformation and sting interference effects with the CAE-AVM test case被引量:7
《Chinese Journal of Aeronautics》2018年第10期1954-1961,共8页Innokentiy KURSAKOV Egor KAZHAN Roy GEBBINK 
supported by the Grant Agreement(No.4.628.21.0004)with the Ministry of Education and Science of the Russian Federation(project unique identifier RFMEFI62815X0004)on the theme‘‘Development and implementation of the optimization of the aircraft power plant aerodynamics as a part of a 3rd generation multidisciplinary optimization and its application to optimization of promising new types of aircraft”
A modern transonic computational fluid dynamics test case is described in this paper,which is the Aerodynamic Validation Model(AVM) from the Chinese Aeronautical Establishment(CAE). The CAE-AVM is a representation...
关键词:Aerodynamic validation model CFD Sting interference Transonic test Wing deformation 
Recent development of a CFD-wind tunnel correlation study based on CAE-AVM investigation被引量:11
《Chinese Journal of Aeronautics》2018年第3期419-428,共10页Jun HUA Sui ZHENG Min ZHONG Ganglin WANG Georg EITELBERG Sinus HEGEN Roy GEBBINK 
supported by the Innovation Funds of AVIC
This paper starts with brief introduction to the open topic of the CFD and wing tunnel correlation study, followed by a description of the Chinese Aeronautical Establishment(CAE) –Aerodynamic Validation Model(AVM...
关键词:Aerodynamic design CFD validation CFD-wind tunnel correlation Model deformation Model support interference 
Correlation analysis of combined and separated effects of wing deformation and support system in the CAE-AVM study被引量:9
《Chinese Journal of Aeronautics》2018年第3期429-438,共10页Min ZHONG Sui ZHENG Ganglin WANG Jun HUA Roy GEBBINK 
The Chinese Aeronautical Establishment(CAE) Aerodynamic Validation Model(AVM)is a dual-purpose test geometry dedicated to verify the aerodynamic performance of a conceptual intercontinental jet aircraft and to pro...
关键词:Aerodynamic validation model CFD CFD-Wind tunnel data correlation Support interference Wing deformation 
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