学者信息

陈荣钱 (RongQian Chen)

航空航天学院

合作者

已发表成果:

WOK 论文 47 篇;中文核心 9 篇;其它论文 3 篇;专利发明 7 个;

  • Linear lattice Boltzmann flux solver with compact third-order finite volume method for acoustic propagation simulations on three-dimensional hybrid unstructured grids

    Computers and Mathematics with Applications,0898-1221,2024-02-15.
    Zhan, Ningyu; Chen, Rongqian; You, Yancheng; Lin, Zelun
    WOS:001152975700001   EI:20240215372119   10.1016/j.camwa.2023.12.003
    收录情况:SCIE、EI
  • A New Sixth-Order Central Weno Scheme for Solving Hyperbolic Conservation Laws

    SSRN,1556-5068,2024-02-13.
    Lin, Zelun (1); Chen, Rongqian (1); Wu, Linkuan (1); You, Yancheng (1)
    EI:20240074020   10.2139/ssrn.4724157
    收录情况:EI
  • Airfoils optimization based on deep reinforcement learning to improve the aerodynamic performance of rotors

    AEROSPACE SCIENCE AND TECHNOLOGY,1270-9638,2023-12.
    Liu, Jiaqi; Chen, Rongqian; Lou, Jinhua; Wu, Hao; You, Yancheng; Chen, Zhengwu
    WOS:001126533300001   10.1016/j.ast.2023.108737
    收录情况:SCIE
  • Three-dimensional high-order finite-volume method based on compact WENO reconstruction with hybrid unstructured grids

    Journal of Computational Physics,0021-9991,2023-10-01.
    Zhan, Ningyu; Chen, Rongqian; You, Yancheng
    WOS:001031793700001   EI:20232714345439   10.1016/j.jcp.2023.112300
    收录情况:SCIE、EI
  • Linear Lattice Boltzmann Flux Solver with Compact Third- Order Finite Volume Method for Acoustic Propagation Simulations on Three-Dimensional Hybrid Unstructured Grids

    SSRN,1556-5068,2023-06-14.
    Zhan, Ningyu (1); Chen, Rongqian (1); You, Yancheng (1)
    EI:20230193817   10.2139/ssrn.4478130
    收录情况:EI
  • Aerodynamic optimization of airfoil based on deep reinforcement learning

    Physics of Fluids,1070-6631,2023-03-01.
    Lou, Jinhua; Chen, Rongqian; Liu, Jiaqi; Bao, Yue; You, Yancheng; Chen, Zhengwu
    WOS:000958363600003   EI:20231313812444   10.1063/5.0137002
    收录情况:SCIE、EI
  • Acoustic multipole source-simplified lattice Boltzmann method for simulating acoustic propagation problems

    INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS,0271-2091,2023-03.
    Chen, Rongqian; Cao, Shuqi; Liu, Wanhong; Song, Qiaochu; You, Yancheng
    WOS:000945334000001   EI:20231213782172   10.1002/fld.5178
    收录情况:SCIE、EI
  • Deep-learning-based aerodynamic shape optimization of rotor airfoils to suppress dynamic stall

    Aerospace Science and Technology,1270-9638,2023-02.
    Liu, Jiaqi; Chen, Rongqian; Lou, Jinhua; Hu, Yue; You, Yancheng
    WOS:000974824100001   EI:20230313381973   10.1016/j.ast.2022.108089
    收录情况:SCIE、EI
  • A Simplified Linearized Lattice Boltzmann Method for Acoustic Propagation Simulation

    ENTROPY,,2022-11.
    Song, Qiaochu; Chen, Rongqian; Cao, Shuqi; Lou, Jinhua; Zhan, Ningyu; You, Yancheng
    WOS:000894921900001   10.3390/e24111622
    收录情况:SCIE
  • An efficient frequency-domain prediction method for aeroacoustic radiation and scattering using equivalent sources

    Journal of Sound and Vibration,0022-460X,2022-09-15.
    Wang, Lican; Chen, Rongqian; You, Yancheng; Wang, Zhaohuan; Song, Qiaochu
    WOS:000813317700002   EI:20222212185911   10.1016/j.jsv.2022.117039
    收录情况:SCIE、EI
  • Linear discrete velocity model-based lattice Boltzmann flux solver for simulating acoustic propagation in fluids

    PHYSICAL REVIEW E,2470-0045,2022-06-21.
    Zhan, Ningyu; Chen, Rongqian; Song, Qiaochu; You, Yancheng
    WOS:000817775600016   EI:20222712324492   10.1103/PhysRevE.105.065303
    收录情况:SCIE、EI
  • Active Flow Control of Helicopter Rotor Based on Coflow Jet

    INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING,1687-5966,2022-06-06.
    Liu, Jiaqi; Chen, Rongqian; Song, Qiaochu; You, Yancheng; Shi, Zheyu
    WOS:000813899400001   EI:20222612268247   10.1155/2022/9299470
    收录情况:SCIE、EI
  • Linear lattice Boltzmann flux solver for simulating acoustic propagation

    COMPUTERS & MATHEMATICS WITH APPLICATIONS,0898-1221,2022-05-15.
    Zhan, Ningyu; Chen, Rongqian; You, Yancheng
    WOS:000805450300002   10.1016/j.camwa.2022.03.034
    收录情况:SCIE
  • Development of a new type of weighted compact scheme

    Journal of Computational Physics,0021-9991,2021-12-01.
    Chen, Rongqian; Wu, Linkuan; You, Yancheng
    WOS:000722654000001   EI:20213610868482   10.1016/j.jcp.2021.110662
    收录情况:SCIE、EI
  • Discrete gas-kinetic scheme-based arbitrary Lagrangian-Eulerian method for moving boundary problems

    Physics of Fluids,1070-6631,2021-06-01.
    Zhan, Ningyu; Chen, Rongqian; You, Yancheng
    WOS:000677520200001   EI:20212410488503   10.1063/5.0051299
    收录情况:SCIE、EI
  • Meshfree lattice Boltzmann flux solver for compressible inviscid flows

    INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS,0271-2091,2021-05.
    Zhan, Ningyu; Chen, Rongqian; Liu, Jiaqi; Qiu, Ruofan; You, Yancheng
    WOS:000588551400001   10.1002/fld.4933
    收录情况:SCIE
  • Meshfree method based on discrete gas-kinetic scheme to simulate incompressible/compressible flows

    PHYSICS OF FLUIDS,1070-6631,2021-01-01.
    Zhan, Ningyu; Chen, Rongqian; You, Yancheng
    WOS:000611029600001   10.1063/5.0033770
    收录情况:SCIE
  • Numerical investigation of dynamic stall suppression of rotor airfoil via improved co-flow jet

    Chinese Journal of Aeronautics,1000-9361,2021.
    Liu, Jiaqi; Chen, Rongqian; You, Yancheng; Shi, Zheyu
    WOS:000865940800001   EI:20214911258846   10.1016/j.cja.2021.07.041
    收录情况:SCIE、EI
  • Aerothermodynamic study of Two-Stage-To-Orbit system composed of wide-speed-range vehicle and rocket

    Acta Astronautica,0094-5765,2021.
    Cheng, Jiaming; Chen, Rongqian; Qiu, Ruofan; Sun, Weiqiang; You, Yancheng
    WOS:000666595000029   EI:20210109720710   10.1016/j.actaastro.2020.11.034
    收录情况:SCIE、EI
  • Study of regular reflection shock waves using a mesoscopic kinetic approach: Curvature pattern and effects of viscosity

    Physics of Fluids,1070-6631,2020-10-01.
    Qiu, Ruofan; Bao, Yue; Zhou, Tao; Che, Huanhuan; Chen, Rongqian; You, Yancheng
    WOS:000586578700001   EI:20204409436709   10.1063/5.0024801
    收录情况:SCIE、EI
  • Generalized form of interpolation-supplemented lattice Boltzmann method for computational aeroacoustics

    Zhejiang Daxue Xuebao (Gongxue Ban)/Journal of Zhejiang University (Engineering Science),1008-973X,2020-08-01.
    Liu, Wan-hong (1); Chen, Rong-qian (1, 2); Qiu, Ruo-fan (1); Lin, Wei (1); You, Yan-cheng (1)
    EI:20203509116582   10.3785/j.issn.1008-973X.2020.08.024
    收录情况:EI
  • Investigation of acoustic propagation and source localization in a hot jet flow

    Journal of Sound and Vibration,0022-460X,2020.
    Wang, Lican; Chen, Rongqian; You, Yancheng; Qiu, Ruofan
    WOS:000595866100002   EI:20204409424069   10.1016/j.jsv.2020.115801
    收录情况:SCIE、EI
  • Study on Dynamic Stall Control of Rotor Airfoil Based on Coflow Jet

    International Journal of Aerospace Engineering,1687-5966,2020.
    Liu, Jiaqi; Chen, Rongqian; Qiu, Ruofan; You, Yancheng; Zhang, Weiguo
    WOS:000603703600001   EI:20210109714003   10.1155/2020/8845924
    收录情况:SCIE、EI
  • Effects of Shear Layer Characteristics on Acoustic Propagation and Source Localization

    Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University,1000-2758,2019-12-01.
    Wang, Lican (1); Chen, Rongqian (1); You, Yancheng (1); Chen, Zhengwu (2); Qiu, Ruofan (1)
    EI:20200207997741   10.1051/jnwpu/20193761148
    收录情况:EI
  • Numerical simulation of flow field under coaxial rigid rotor/fuselage interaction

    Hangkong Dongli Xuebao/Journal of Aerospace Power,1000-8055,2019-11-01.
    Liu, Jiaqi (1); Chen, Rongqian (1); Cheng, Jiaming (1); Lin, Wei (1); You, Yancheng (1)
    EI:20195207925317   10.13224/j.cnki.jasp.2019.11.009
    收录情况:EI
  • A unified correction method for the acoustic refraction (UCMAR) caused by a three dimensional shear layer

    Acta Acustica united with Acustica,1610-1928,2019.
    Wang, Lican (1); Chen, Rongqian (1); You, Yancheng (1); Wu, Wenjun (2); Qiu, Ruofan (1)
    WOS:000499974400002   EI:20194707725302   10.3813/AAA.919353
    收录情况:SCIE、EI
  • Compressible lattice Boltzmann simulations on high-performance and low-cost GeForce GPU

    Concurrency Computation,1532-0626,2019.
    Qiu, Ruo-Fan (1); Wang, Hai-Ning (2); Zhu, Jian-Feng (1); Chen, Rong-Qian (1); Zhu, Cheng-Xiang (1)...
    WOS:000489324000009   EI:20192206972463   10.1002/cpe.5341
    收录情况:SCIE、EI
  • Numerical Simulation of Aerodynamic Characteristics of Helicopter Rotor with Tip Slots

    Transactions of Nanjing University of Aeronautics and Astronautics,1005-1120,2018-12-01.
    Chen, Rongqian (1); Wang, Xu (2); Cheng, Qiyou (3); Zhu, Chengxiang (1); You, Yancheng (1)
    EI:20192006931019  
    收录情况:EI
  • Direct numerical simulation of sheet breakup formed by two impinging jets with non-Newtonian shear thinning properties

    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,1000-6893,2018-05-25.
    Zhu, Chengxiang (1); Wu, Meng (1); Chen, Rongqian (1); You, Yancheng (1)
    EI:20183605785161   10.7527/S1000-6893.2018.21982
    收录情况:EI
  • A Hermite-based lattice Boltzmann model with artificial viscosity for compressible viscous flows

    INTERNATIONAL JOURNAL OF MODERN PHYSICS B,0217-9792,2018-05-20.
    Qiu, RF; Chen, RQ; Zhu, CX; You, YC
    WOS:000431992000007   10.1142/S0217979218501576
    收录情况:SCIE
  • A double-distribution-function lattice Boltzmann model for high-speed compressible viscous flows

    Computers and Fluids,0045-7930,2018-04-30.
    Qiu, Ruo-Fan(1); Zhu, Cheng-Xiang(1); Chen, Rong-Qian(1); Zhu, Jian-Feng(1); You, Yan-Cheng(1)
    WOS:000429513000003   EI:20180604763214   10.1016/j.compfluid.2018.01.039
    收录情况:SCIE、EI
  • Pre-Injection of Cracked Hydrocarbon Fuel in Hypersonic Inlets

    Tuijin Jishu/Journal of Propulsion Technology,1001-4055,2018-01-01.
    Zhu, Cheng-Xiang(1); Huang, Yu-Rou(1); Chen, Rong-Qian(1); You, Yan-Cheng(1)
    EI:20181705041909   10.13675/j.cnki.tjjs.2018.01.022
    收录情况:EI
  • Investigation of adaptive slot control method for starting characteristics of hypersonic inlets

    Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering,0954-4100,2018.
    Zhu, Chengxiang (1); Yang, Rijiong (1); Chen, Rongqian (1); Qiu, Ruofan (1); You, Yancheng (1)
    WOS:000481443000029   EI:20190606483330   10.1177/0954410018819523
    收录情况:SCIE、EI
  • Three-dimensional coupled double-distribution-function lattice Boltzmann models for compressible Navier-Stokes equations

    PRAMANA-JOURNAL OF PHYSICS,0304-4289,2017-12.
    Qiu, Ruo-Fan; You, Yan-Cheng; Zhu, Cheng-Xiang; Chen, Rong-Qian; Zhu, Jian-Feng
    WOS:000418076400011   EI:20194807746559   10.1007/s12043-017-1480-2
    收录情况:SCIE、EI
  • Direct numerical simulation of impinging jet breakup with non-Newtonian properties at low Weber number

    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,1000-6893,2017-08-25.
    Zhu, Chengxiang(1); Chen, Rongqian(1); You, Yancheng(1)
    EI:20174204277806   10.7527/S1000-6893.2017.120764
    收录情况:EI
  • Lattice Boltzmann simulation for high-speed compressible viscous flows with a boundary layer

    Applied Mathematical Modelling,0307-904X,2017-08.
    Qiu, Ruo-Fan(1); You, Yan-Cheng(1); Zhu, Cheng-Xiang(1); Chen, Rong-Qian(1)
    WOS:000403994400031   EI:20172303740551   10.1016/j.apm.2017.03.016
    收录情况:SCIE、EI
  • An implicit-explicit finite-difference lattice Boltzmann subgrid method on nonuniform meshes

    INTERNATIONAL JOURNAL OF MODERN PHYSICS C,0129-1831,2017-04.
    Qiu, Ruofan; Chen, Rongqian; You, Yancheng
    WOS:000400271700003   10.1142/S0129183117500450
    收录情况:SCIE
  • Injection and Mixing Performance in an Elliptical Scramjet Combustor

    Tuijin Jishu/Journal of Propulsion Technology,1001-4055,2017-03-01.
    Zhou, Xun-Huang(1); Chen, Rong-Qian(1); Li, Yi-Qing(1); Teng, Jian(1); You, Yan-Cheng(1)
    EI:20172303738840   10.13675/j.cnki.tjjs.2017.03.020
    收录情况:EI
  • Analysis on the performance of a hypersonic inward turning inlet with three combined channels

    Proceedings of the International Astronautical Congress, IAC,0074-1795,2017.
    Zhu, Chengxiang (1); Wu, Meng (1); Qiu, Ruofan (1); Chen, Rongqian (1); You, Yancheng (1)
    EI:20183305702286  
    收录情况:EI
  • Lattice boltzmann simulation for supersonic/hypersonic compressible flows

    21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017,,2017.
    Qiu, Ruofan(1); You, Yanchen(1); Zhu, Chengxiang(1); Chen, Rongqian(1)
    EI:20171603581533  
    收录情况:EI
  • Numerical investigation of fuel pre-injection with different injector configurations in hypersonic inlet

    21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017,,2017.
    Zhu, Chengxiang(1); Qiu, Ruofan(2); Chen, Rongqian(2); You, Yancheng(1)
    EI:20171603581679  
    收录情况:EI
  • Effects of the chemical nonequilibrium flow on the performance of three dimensional expansion nozzle

    21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017,,2017.
    Chen, Rongqian(1); Wang, Lican(1); Xing, Fei(1); Zhu, Chengxiang(1); You, Yancheng(1)
    EI:20171603581558  
    收录情况:EI
  • Inverse method of characteristics with given exit parameters for the computation of supersonic flows

    21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017,,2017.
    Zhu, Chengxiang(1); Qiu, Ruofan(2); Chen, Rongqian(2); You, Yancheng(1)
    EI:20171603581578  
    收录情况:EI
  • A new understanding of hypersonic inlets' startability criterion

    Tuijin Jishu/Journal of Propulsion Technology,1001-4055,2016-11-01.
    Pan, Cheng-Jian(1,2); Shi, Chong-Guang(1); Li, Yi-Qing(1); You, Yan-Cheng(1); Chen, Rong-Qian(1)
    EI:20164903092905   10.13675/j.cnki.tjjs.2016.11.006
    收录情况:EI
  • Numerical simulation of nacelle's effects on propeller slipstream based on IDDES model

    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,1000-6893,2016-06-25.
    Chen, Rongqian(1); Wang, Xu(1); You, Yancheng(1)
    EI:20162802571820   10.7527/S1000-6893.2015.0353
    收录情况:EI
  • Effects of incoming boundary layer on injection characteristics of a scramjet combustor

    Hangkong Dongli Xuebao/Journal of Aerospace Power,1000-8055,2016-06-01.
    Zhou, Xun-Huang(1); Chen, Rong-Qian(1); You, Yan-Cheng(1); Zhu, Cheng-Xiang(1); Huang, Yue(1)
    EI:20162702553813   10.13224/j.cnki.jasp.2016.06.010
    收录情况:EI
  • Integration methodology for waverider-derived hypersonic inlet and vehicle forebody

    AIAA AVIATION 2014 -19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference,,2014.
    Li, Yiqing(1); An, Ping(1); Pan, Chengjian(1); Chen, Rongqian(1); You, Yancheng(1)
    EI:20143818170110  
    收录情况:EI
  • 通用的插值补充格子Boltzmann方法应用于计算气动声学

    浙江大学学报(工学版),1008-973X,2020-08-06.
    刘万鸿;陈荣钱;邱若凡;林威;尤延铖
    CSCD核心
  • 剪切层形态对声波传播与声源定位的影响研究

    西北工业大学学报,1000-2758,2019-12-15.
    王李璨;陈荣钱;尤延铖;陈正武;邱若凡
    CSCD核心
  • 剪切稀化非牛顿射流撞击液膜破碎直接数值模拟

    航空学报,1000-6893,2018.
    朱呈祥;吴猛;陈荣钱;尤延铖
    CSCD核心
  • 桨尖开孔参数对旋翼流场特性的影响研究

    西北工业大学学报,1000-2758,2018.
    陈荣钱;王旭;程起有;朱呈祥;尤延铖
    CSCD核心
  • 高超声速进气道的裂解碳氢燃料提前喷注研究

    推进技术,1001-4055,2018.
    朱呈祥;黄雨柔;陈荣钱;尤延铖
    CSCD核心
  • 低韦伯数非牛顿射流撞击破碎直接数值模拟

    航空学报,1000-6893,2017-08-25.
    朱呈祥;陈荣钱;尤延铖
    CSCD核心
  • 高超声速进气道起动问题的理论判据新认识

    推进技术,1001-4055,2016-10-12.
    潘成剑;施崇广;李怡庆;尤延铖;陈荣钱
    CSCD核心 CSCD核心 理工二类核心
  • 考虑来流边界层的超燃燃烧室喷射特性

    航空动力学报,1000-8055,2016-06-08.
    周驯黄;陈荣钱;尤延铖;朱呈祥;黄玥
    CSCD核心 CSCD核心
  • 短舱对螺旋桨滑流影响的IDDES数值模拟

    航空学报,1000-6893,2016-01-25.
    陈荣钱;王旭;尤延铖
    CSCD核心 CSCD核心
  • 椭圆形超燃燃烧室内燃料喷射和掺混性能研究

    推进技术,10014055,2017-03-01.
    周驯黄;陈荣钱;李怡庆;滕健;尤延铖
  • 高超声速进气道的裂解碳氢燃料提前喷注

    第九届全国流体力学学术会议论文摘要集,,2016-10-20.
    朱呈祥;陈荣钱;尤延铖
  • 非牛顿撞击射流破碎的直接数值模拟

    中国航天第三专业信息网第三十七届技术交流会暨第一届空天动力联合会议论文集,,2016-08-17.
    朱呈祥;陈荣钱;尤延铖