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CONFIGURATION: 作品数：936被引量：1385H指数：13; 导出分析报告; 相关作者：傅恒志杨劼人黄锋郭景杰苏彦庆更多>>; 相关机构：南京航空航天大学上海交通大学清华大学中国科学院更多>>; 相关期刊：更多>>; 相关基金：国家自然科学基金国家重点基础研究发展计划国家高技术研究发展计划国家教育部博士点基金更多>>

Design and optimization of origami-inspired inflatable deployable tubular structures: 《Chinese Journal of Aeronautics》2025年第3期645-661,共17页Bo QIN Shengnan LYU Shiwei LIU Xilun DING; supported by the National Natural Science Foundation of China(No.52222501,52075016,52192632);the Fundamental Research Funds for the Central Universities(Grant No.YWF-23-L-904).; Inflatable deployable structures inspired by origami have significant applications in space missions such as solar arrays and antennas.In this paper,a generalized Miura-ori tubular cell(GMTC)is presented as the basic ...; 关键词：Rigid origamil Inflatable deployable structure Variable volume Multistable configuration Parametric optimization design

Aero-propulsion analysis of distributed ducted-fan propulsion based on lifting-line driven body-force model: 《Chinese Journal of Aeronautics》2025年第2期60-74,共15页Hanru LIU Xingyu ZHAO Fang ZHOU Yuyao FENG Yangang WANG; the funding support from the Taihang Laboratory,China(No.D2024-1-0201).; As the environmental problems become increasingly serious,distributed electrical propulsion systems with higher aerodynamic efficiency and lower pollution emission have received extensive attention in recent years.The...; 关键词：Ducted fan Distributed electrical PROPULSION Lifting line theory Body force method Aero-propulsion integrated CONFIGURATION

Configuration uncertainty propagation of gravitational-wave observatory using a directional state transition tensor: 《Chinese Journal of Aeronautics》2024年第12期174-191,共18页Dong QIAO Xingyu ZHOU Xiangyu LI; supported by the National Key R&D Program of China(No.2020YFC2201200).; Configuration stability is essential for a space-based Gravitational-Wave(GW)observatory,which can be impacted by orbit insertion uncertainties.Configuration uncertainty propagation is vital for investigating the infl...; 关键词：Space-based gravitational wave observatory Configuration stability Configuration uncertainty propagation State transition tensor Feasible domain Uncertainty analysis SPACECRAFT

Aero-structural design of joined-wing aircraft based on high-fidelity model: 《Chinese Journal of Aeronautics》2024年第4期363-377,共15页Cheng HE Fengjiang ZHAN Luchuang MA Gang CHEN Jianying MA; supported by the Fundamental Research FundsfortheCentralUniversities,China(No. 56XCA2205402)。; The joined-wing configuration reduces induced drag and structural weight by connecting the rear wing to the front wing.In addition,the rear wing can replace the role of the horizontal tail of a conventional aircraft,t...; 关键词：Joined-wing configuration Aircraft design Aero-structural design Finite element Wind tunnel test

Effect of longitudinal lift distribution on sonic boom of a canard-wing-stabilator-body configuration被引量：1: 《Chinese Journal of Aeronautics》2023年第6期92-108,共17页Liwen ZHANG Zhonghua HAN Jianling QIAO Wenping SONG Yulin DING Xuehe WANG; sponsored by the National Natural Science Foundation of China(Nos.12072285,U20B2007);the Shaanxi Science Fund for Distinguished Young Scholars,China(No.2020JC-13);the Natural Science Funding of Shaanxi Province,China(No.2020JM-127).; After the last flight of the Concorde in 2003,sonic boom has been one of the obstacles to the return of a supersonic transport aircraft to service.To reduce the sonic boom intensity to an acceptable level,it is of gre...; 关键词：Computational fluid dynamics Longitudinal lift distribution Sonic boom Sonic boom reduction Supersonic transport

Symmetric Mach reflection configuration with asymmetric unsteady solution: 《Chinese Journal of Aeronautics》2023年第4期75-78,共4页Chenyuan BAI Miaomiao WANG Ziniu WU; supported partly by the National Key Project,China(No.GJXM92579);the National Science and Technology Major Project,China(No.2017-II-003-0015);the National Natural Science Foundation of China(Nos.11721202,52192632);the Young Elite Scientists Sponsorship Program of CAST,Young Talent Support Plan of Beihang University.; Symmetric Mach reflection in steady supersonic flow has been usually studied by solving a half-plane problem with the symmetric line treated as reflecting surface,thus losing the opportunity to discover antisymmetric ...; 关键词：Antisymmetric solution Mach reflection Shock reflection Supersonic flow

Transitional wave configurations between Type Ⅲ and Type Ⅳ oblique-shock/bow-shock interactions被引量：2: 《Chinese Journal of Aeronautics》2023年第3期96-106,共11页Jun PENG Shuai LI Fan YANG Mingyue LIN Guilai HAN Zongmin HU; co-supported by the National Key Research and Development Plan of China(No.2019YFA0405204);the National Natural Science Foundation of China(Nos.12172365,12072353 and 12132017)。; The interactions of oblique/bow shock waves are the key flow phenomena restricting the design and aerothermodynamic performance of high-speed vehicles.Type Ⅲ and Type Ⅳ Shock/Shock Interactions(SSIs)have been extens...; 关键词：Shock interactions Transitional configuration Aerodynamic heating Shear layer Mach interaction

Optimization of fixed aviation support resource station configuration for aircraft carrier based on aircraft dispatch mission scheduling被引量：7: 《Chinese Journal of Aeronautics》2023年第2期127-138,共12页Yujie LIU Wei HAN Xichao SU Rongwei CUI; Before the dispatch of the carrier-based aircraft,a series of pre-flight preparation operations need to be completed on the flight deck.Flight deck fixed aviation support resource station configuration has an importan...; 关键词：Carrier-based aircraft Multi-objective optimization Resource configuration SCHEDULING Variable neighborhood search

Coordinated attitude control for flexible spacecraft formation with actuator configuration misalignment被引量：1: 《Chinese Journal of Aeronautics》2021年第3期176-186,共11页Xiaomei CHENG Yuan LIU Yi QIN Feng WANG Junjie ZHANG; supported by the National Natural Science Foundation of China(Nos.61833009,61690212 and 51875119);the National Key Research and Development Project(No.2016YFB0501203)。; This paper investigates the coordinated attitude control problem for flexible spacecraft formation with the consideration of actuator configuration misalignment.First,an integral-type sliding mode adaptive control law...; 关键词：Actuator configuration misalignment Adaptive control Attitude control Integral-type sliding mode control Spacecraft formation flying

Numerical simulation of broken pin effects on the flow field and cooling performance of a double-wall cooling configuration: 《Chinese Journal of Aeronautics》2021年第2期358-375,共18页Wenjing GAO Honglin LI Lei LI Zhe’nan ZHAO Zhufeng YUE; supported by the National Natural Science Foundation of China (No. 51975471);Aviation Power Foundation of China (No. 6141B090319);Natural Science Basic Research Plan in Shaanxi Province of China (No.2018JM5173);National Natural Science Foundation of China(No. 51975471);National Science and Technology Major Project (2017-VIII-0003-0114);Natural Science Foundation of Shaanxi Province (No. 2018JQ5041)。; In this paper, the flow characteristics of the double wall structure are presented and the effect of the broken pin size on the cooling performance and flow field of the double wall configuration is investigated. A pe...; 关键词：Broken pin Computational Fluid Dynamics Cooling performance Double wall configuration Turbine blades

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