厦门大学学者库

学者信息

朱呈祥 (ChengXiang Zhu)

航空航天学院

归档
2024
2023
2022
2021
2020
合作者

已发表成果：

WOK 论文 54 篇;中文核心 28 篇;其它论文 10 篇;专利发明 8 个;图书及章节 1 本;

  • Conceptual design methodology and performance evaluation of turbine-based combined cycle inward-turning inlet with twin-design points

    Aerospace Science and Technology,1270-9638,2024-09.
    Hu, Zhancang; Li, Zhonglong; Tang, Yiqi; Yu, Yaokun; Zhang, Yuchao; Zheng, Xiaogang; Zhu, Chengxian...
    WOS:001282525200001   EI:20242716598795   10.1016/j.ast.2024.109309
    收录情况：SCIE、EI

  • Fully appreciating the impossibility of shock wave regular reflection from the axis of symmetry in axisymmetric internal flows

    Physics of Fluids,1070-6631,2024-07-01.
    Zhang, Tao (1); Hu, Waner (1); Da, Xingya (2); Shi, Chongguang (1); Zhu, Chengxiang (1); You, Yanch...
    EI:20242916718760   10.1063/5.0220314
    收录情况：EI

  • Analytical reconstruction of axisymmetric curved shock wave/boundary layer interactions

    Physics of Fluids,1070-6631,2024-04-01.
    Cheng, Jianrui; Zhang, Tao; Shi, Chongguang; Da, Xingya; Zhu, Chengxiang; You, Yancheng
    WOS:001209401100014   EI:20241916033334   10.1063/5.0199292
    收录情况：SCIE、EI

  • Machine Learning-Based Backpressure Unstart Prediction and Warning Method for Combined Cycle Engine Hypersonic Inlet-Oriented Wide Speed Range

    INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING,1687-5966,2024-02-29.
    Min, Ke; Hong, Tanbao; Cai, Zejun; Yu, Lianchen; Zhu, Chengxiang; Zeng, Jianping
    WOS:001180461500002   EI:20241115752132   10.1155/2024/2284914
    收录情况：SCIE、EI

  • Conceptual Design Methodology and Performance Evaluation of Inward-Turning Tbcc Inlet with Twin-Design Points

    SSRN,1556-5068,2024-02-15.
    Hu, Zhancang (1); Li, Zhonglong (2); Tang, Yiqi (1); Yu, Yaokun (1); Zhang, Yuchao (2); Zheng, Xiao...
    EI:20240080267   10.2139/ssrn.4727097
    收录情况：EI

  • A constant pressure differential valve and its controlling characteristics for aero engine

    FLOW MEASUREMENT AND INSTRUMENTATION,0955-5986,2024-02.
    Cai, Huikun; Lu, Yidong; Xu, Chen; You, Yancheng; Zhu, Chengxiang
    WOS:001145182400001   10.1016/j.flowmeasinst.2023.102507
    收录情况：SCIE

  • An Analysis Method to Identify the Importance of Technical Parameters for Complex Products

    Mechanisms and Machine Science,2211-0984,2024.
    Sun, Wang (1); Chen, Jinhao (1); Guo, Xiaoxuan (1); Zhu, Chengxiang (1); You, Yancheng (1); Mu, Rui...
    EI:20243016753746   10.1007/978-981-97-0922-9_11
    收录情况：EI

  • Mach reflection of three-dimensional curved shock waves on V-shaped blunt leading edges

    JOURNAL OF FLUID MECHANICS,0022-1120,2023-11-22.
    Zhang, Tao; Cheng, Jianrui; Shi, Chongguang; Zhu, Chengxiang; You, Yancheng
    WOS:001105819000001   EI:20235115258871   10.1017/jfm.2023.866
    收录情况：SCIE、EI

  • Reflection and transition of planar curved shock waves

    Journal of Fluid Mechanics,0022-1120,2023-03-25.
    Zhang, Tao; Xu, Kejing; Shi, Chongguang; Zhu, Chengxiang; You, Yancheng
    WOS:000952431700001   EI:20231213782219   10.1017/jfm.2023.132
    收录情况：SCIE、EI

  • Analytical model for curved-shock Mach reflection

    Physics of Fluids,1070-6631,2023-03.
    Shi, Chongguang; You, Yancheng; Zheng, Xiaogang; Zhu, Chengxiang
    WOS:000942071400003   EI:20231013681233   10.1063/5.0139784
    收录情况：SCIE、EI

  • Analytical model for predicting the length scale of shock/boundary layer interaction with curvature (vol 34, 111701, 2022)

    Physics of Fluids,1070-6631,2023-03.
    Cheng, Jianrui; Yang, Kai; Zheng, Xiaogang; Shi, Chongguang; Zhu, Chengxiang; You, Yancheng
    WOS:000944031400002   EI:20231113740412   10.1063/5.0147923
    收录情况：SCIE、EI

  • Multi-ducted twin-turbines ejector-ramjet/scramjet combined cycle engine for hypersonic civil vehicles

    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,1000-6893,2023-01-25.
    Yin, Zeyong (1, 2); You, Yancheng (2); Zhu, Chengxiang (2); Zhu, Jianfeng (2); Wu, Liaoni (2); Huan...
    EI:20230713592481   10.7527/S1000-6893.2022.27181
    收录情况：EI

  • Thermal insulation characteristics of high-temperature heat seals for hypersonic aero-engines

    Journal of Physics: Conference Series,1742-6588,2023.
    Li, Haiping (1); Cai, Huikun (1); Du, Zhihong (1); You, Yancheng (1); Zhu, Chengxiang (1)
    EI:20233914797212   10.1088/1742-6596/2566/1/012119
    收录情况：EI

  • Digital Twin System for Propulsion Design of UAVs

    Proceedings - VRCAI 2022: 18th ACM SIGGRAPH International Conference on Virtual-Reality Continuum and its Applications in Industry,,2022-12-27.
    Wang, Zexi (1); Chen, Pan (1); Qin, Yajie (1); Xie, Jingsi (1); Wang, Ying (1); Luo, Bin (1); Zhu, ...
    EI:20230613550320   10.1145/3574131.3574464
    收录情况：EI

  • Analytical model for predicting the length scale of shock/boundary layer interaction with curvature

    Physics of Fluids,1070-6631,2022-11-01.
    Cheng, Jianrui; Yang, Kai; Zheng, Xiaogang; Shi, Chongguang; Zhu, Chengxiang; You, Yancheng
    WOS:000890878500029   EI:20225013226437   10.1063/5.0125439
    收录情况：SCIE、EI

  • Inverse Design of Hypersonic Waveriders with Variable Cross-Section Shock Waves

    JOURNAL OF SPACECRAFT AND ROCKETS,0022-4650,2022-11.
    Wang, Xiao; Zheng, Xiaogang; Zhu, Chengxiang; You, Yancheng
    WOS:000912119400001   EI:20230513461397   10.2514/1.A35434
    收录情况：SCIE、EI

  • The Cluster Design and Redox Behavior Characterization of Polyoxometalates for Redox Flow Batteries

    CHEMISTRY-AN ASIAN JOURNAL,1861-4728,2022-11.
    Han, Yanhong; Lan, Jinji; Li, Ke; Yang, Le; Zhu, Chengxiang; Chen, Jiajia
    WOS:000883114700001   EI:20224913211586   10.1002/asia.202200950
    收录情况：SCIE、EI

  • Theoretical model of 2D curved shock wave/turbulent boundary layer interaction

    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,1000-6893,2022-09-25.
    Cheng, Jianrui (1); Shi, Chongguang (1); Qu, Lixia (2); Xu, Yue (2); You, Yancheng (1); Zhu, Chengx...
    EI:20224613128442   10.7527/S1000-6893.2021.25993
    收录情况：EI

  • Design of multistage compression waverider based on the local-turning osculating cones method

    Lixue Xuebao/Chinese Journal of Theoretical and Applied Mechanics,0459-1879,2022-03-18.
    Zheng, Xiaogang (1); Zhu, Chengxiang (1); You, Yancheng (1)
    EI:20221511958488   10.6052/0459-1879-21-357
    收录情况：EI

  • Design of Multi-channel Pressure Data Acquisition System Based on Resonant Pressure Sensor for FADS

    Lecture Notes in Electrical Engineering,1876-1100,2022.
    Fan, Xianguang (1); Mao, Hailing (1); Zhu, Chengxiang (1); Wu, Juntao (1); Xu, Yingjie (1); Wang, X...
    EI:20223112465960   10.1007/978-981-19-2456-9_46
    收录情况：EI

  • Integration Layout of Double-Modules Chin Inward-Turning Inlet and Conical Forebody

    Tuijin Jishu/Journal of Propulsion Technology,1001-4055,2021-11.
    Yang, Ri-Jiong (1); Zheng, Xiao-Gang (1); Shi, Chong-Guang (1); Li, Yi-Qing (1, 2); Zhu, Cheng-Xian...
    EI:20214611143658   10.13675/j.cnki.tjjs.200276
    收录情况：EI

  • Method of curved-shock characteristics with application to inverse design of supersonic flowfields

    JOURNAL OF FLUID MECHANICS,0022-1120,2021-06-14.
    Shi, Chongguang; Zhu, Chengxiang; You, Yancheng; Zhu, Guangsheng
    WOS:000661196800001   EI:20212510521812   10.1017/jfm.2021.454
    收录情况：SCIE、EI

  • Analysis of Effects of Mode Transition Type on Performance of Mode Transition for 3D Inward-Turning Combined Inlet

    Tuijin Jishu/Journal of Propulsion Technology,1001-4055,2020-12.
    Hu, Zhan-Cang (1); Cai, Ze-Jun (1); Wang, Tian-Yang (1); Zhu, Cheng-Xiang (1); Wu, Liao-Ni (1); You...
    EI:20210309770940   10.13675/j.cnki.tjjs.190875
    收录情况：EI

  • Direct Numerical Simulation of Breakup Characteristics of Power Law Fluid Impingement Jet

    Tuijin Jishu/Journal of Propulsion Technology,1001-4055,2020-08-01.
    Zheng, Hao-Ming (1); Sun, Jun-Ning (1); Zhu, Cheng-Xiang (1); You, Yan-Cheng (1)
    EI:20203709165066   10.13675/j.cnki.tjjs.190537
    收录情况：EI

  • Local-Turning Osculating Cones Method for Waverider Design

    AIAA JOURNAL,0001-1452,2020-08.
    Zheng, Xiaogang; Hu, Zhancang; Li, Yiqing; Zhu, Chengxiang; You, Yancheng; Song, Wenjia
    WOS:000560023000021   10.2514/1.J059139
    收录情况：SCIE

  • Multiple Osculating Cones' Waverider Design Method for Ruled Shock Surfaces

    AIAA JOURNAL,0001-1452,2020-02.
    Zheng, Xiaogang; Li, Yiqing; Zhu, Chengxiang; You, Yancheng
    WOS:000513533200028   EI:20201108281454   10.2514/1.J058640
    收录情况：SCIE、EI

  • Second-order curved shock theory

    Journal of Fluid Mechanics,0022-1120,2020.
    Shi, Chongguang; Han, Weiqiang; Deiterding, Ralf; Zhu, Chengxiang; You, Yancheng
    WOS:000525277900001   EI:20201408366498   10.1017/jfm.2020.158
    收录情况：SCIE、EI

  • Local-turning osculating cones method for waverider design

    AIAA Journal,0001-1452,2020.
    Zheng, Xiaogang (1); Hu, Zhancang (1); Li, Yiqing (2); Zhu, Chengxiang (1); You, Yancheng (1); Song...
    EI:20203309039289   10.2514/lJ059139
    收录情况：EI

  • Analysis on the Low Speed Performance of an Inward-Turning Multiduct Inlet for Turbine-Based Combined Cycle Engines

    INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING,1687-5966,2019-12-07.
    Zhu, CX; Zhang, HF; Hu, ZC; You, YC
    WOS:000503506600002   EI:20200107951334   10.1155/2019/6728387
    收录情况：SCIE、EI

  • Experimental Study of TBCC Engine Performance in Low Speed Wind Tunnel

    Tuijin Jishu/Journal of Propulsion Technology,1001-4055,2019-11-01.
    Guo, Feng (1); Gui, Feng (2); You, Yan-Cheng (1); Zhu, Jian-Feng (1); Zhu, Cheng-Xiang (1)
    EI:20195207901133   10.13675/j.cnki.tjjs.180667
    收录情况：EI

  • Direct numerical simulation of impinging jet with non-Newtonian shear thinning properties at high ambient pressure

    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,1000-6893,2019-06-25.
    Zhu, Chengxiang (1); Zheng, Haoming (1); You, Yancheng (1)
    EI:20193207285586   10.7527/S1000-6893.2019.22783
    收录情况：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

  • Aerodynamic Combination Design Concept for Hypersonic Waverider Forebody and Inward Turning Inlet

    Tuijin Jishu/Journal of Propulsion Technology,1001-4055,2018-10-01.
    Li, Yi-Qing (1); Shi, Chong-Guang (1); Zhu, Cheng-Xiang (1); You, Yan-Cheng (1)
    EI:20190206361739   10.13675/j.cnki.tjjs.2018.10.016
    收录情况：EI

  • Reversal design of external compression bump of Bump inlet based on osculating cones principle

    Hangkong Dongli Xuebao/Journal of Aerospace Power,1000-8055,2018-09-01.
    Zheng, Xiaogang (1); Li, Yiqing (1); Ouyang, Zhixian (1); Zhu, Chengxiang (1); You, Yancheng (1)
    EI:20184806135364   10.13224/j.cnki.jasp.2018.09.024
    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

  • Integration design and analysis for curved conical forebody and three-dimensional inward turning inlet

    Hangkong Dongli Xuebao/Journal of Aerospace Power,1000-8055,2018-01-01.
    Li, Yiqing(1); Zhou, Xunhuang(1); Zhu, Chengxiang(1); You, Yancheng(1)
    EI:20181905145732   10.13224/j.cnki.jasp.2018.01.011
    收录情况：EI

  • An inverse design tool for two-dimensional blade generation in aerospace engineering education

    Computer Applications in Engineering Education,1061-3773,2018.
    Zhu, Chengxiang (1); Li, Mingfeng (1); Shi, Chongguang (1); You, Yancheng (1)
    WOS:000460354700009   EI:20184706113658   10.1002/cae.22082
    收录情况：SCIE、EI

  • Design of a Three-Dimensional Hypersonic Inward-Turning Inlet with Tri-Ducts for Combined Cycle Engines

    INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING,1687-5966,2018.
    Zhu, CX; Zhang, X; Kong, F; You, YC
    WOS:000452991600001   EI:20191106619583   10.1155/2018/7459141
    收录情况：SCIE、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

  • 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

  • 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

  • Direct numerical simulation of a non-Newtonian liquid jet in crossflow

    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,1000-6893,2016-09-25.
    Zhu, Chengxiang(1); You, Yancheng(1)
    EI:20163902850728   10.7527/S1000-6893.2016.0004
    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

  • An inverse method for supersonic flowfield with given downstream boundary

    Tuijin Jishu/Journal of Propulsion Technology,1001-4055,2016-04-01.
    Han, Wei-Qiang(1); Zhu, Cheng-Xiang(1); You, Yan-Cheng(1); Li, Yi-Qing(1)
    EI:20162102408061   10.13675/j.cnki.tjjs.2016.04.004
    收录情况：EI

  • 考虑巡航攻角的三维内转进气道设计与分析

    航空学报,1000-6893,2024-12-02.
    郑晓刚;胡占仓;蔡泽君;施崇广;朱呈祥;尤延铖
    CSCD核心库

  • 高超声速三维内转进气道研究进展综述

    航空学报,1000-6893,2024-12-02.
    郑晓刚;施崇广;张加乐;张咪;朱文磊;朱呈祥;尤延铖
    CSCD核心库

  • 基于NSGA-III-SAM算法的冲压发动机喷管性能预测

    航空学报,1000-6893,2024-08-21.
    闵科;蔡泽君;张加乐;朱呈祥
    CSCD核心库

  • 侧滑角对V型钝化唇口激波干扰结构影响研究

    航空学报,1000-6893,2024-06-30.
    饶洛瑜;张涛;施崇广;朱呈祥;尤延铖
    CSCD核心库

  • 三维弯曲流面法及其在外流乘波体中的应用

    航空学报,1000-6893,2024-06-19.
    杨凯;张勐飞;施崇广;余耀堃;郑晓刚;朱呈祥;尤延铖
    CSCD核心库

  • 基于局部偏转吻切方法的背部进气高超飞行器一体化设计研究

    空天技术,2097-0714,2023-10-15.
    郑晓刚;林德寿;方啸雷;尤延铖;朱呈祥
    CSCD核心库

  • 基于三维弯曲激波的宽域变马赫数乘波体设计分析

    南京航空航天大学学报,1005-2615,2022-10-15.
    尤延铖;郑晓刚;丁晓婷;汤祎麒;朱呈祥
    CSCD核心

  • 面向高超民机的多通道双涡轮引射冲压组合动力研究

    航空学报,1000-6893,2022-06-21.
    尹泽勇;尤延铖;朱呈祥;朱剑锋;吴了泥;黄玥
    CSCD核心

  • 面向高超声速民机的多通道双涡轮引射冲压组合动力

    航空学报,1000-6893,2022-06-21.
    尹泽勇;尤延铖;朱呈祥;朱剑锋;吴了泥;黄玥
    CSCD核心

  • 基于局部偏转吻切方法的多级压缩乘波体设计

    力学学报,0459-1879,2022-03-18.
    郑晓刚;朱呈祥;尤延铖
    CSCD核心

  • XTER内收缩组合进气道设计理念及气动特性

    空气动力学学报,0258-1825,2022-02-15.
    蔡泽君;胡占仓;余联郴;洪唐宝;朱呈祥;尤延铖
    CSCD核心

  • 二维弯曲激波/湍流边界层干扰流动理论建模

    航空学报,1000-6893,2021-09-24.
    程剑锐;施崇广;瞿丽霞;徐悦;尤延铖;朱呈祥
    CSCD核心

  • 双模块下颌式内转进气道/圆锥前体一体化布局研究

    推进技术,1001-4055,2020-10-21.
    杨日炯;郑晓刚;施崇广;李怡庆;朱呈祥;尤延铖
    CSCD核心

  • 转级模式对三维内转组合进气道模态转换性能的影响分析

    推进技术,1001-4055,2020-06-30.
    胡占仓;蔡泽君;王天洋;朱呈祥;吴了泥;尤延铖
    CSCD核心

  • 幂律型流体撞击射流破碎特性直接数值模拟

    推进技术,1001-4055,2019-12-18.
    郑浩铭;孙俊柠;朱呈祥;尤延铖
    CSCD核心

  • 曲锥前体/内转进气道一体化设计与试验研究

    实验流体力学,1672-9897,2019-10-15.
    郑晓刚;李中龙;李怡庆;张旭;朱呈祥;尤延铖
    CSCD核心

  • 一种涡轮基组合动力的整机低速风洞试验研究

    推进技术,1001-4055,2019-06-11.
    郭峰;桂丰;尤延铖;朱剑锋;朱呈祥
    CSCD核心

  • 高压环境下剪切稀化非牛顿撞击射流直接数值模拟

    航空学报,1000-6893,2019-03-04.
    朱呈祥;郑浩铭;尤延铖
    CSCD核心

  • 高压环境下剪切稀化非牛顿撞击射流直接数值模拟

    航空学报,1000-6893,2019-03-04.
    朱呈祥;郑浩铭;尤延铖
    CSCD核心

  • 曲锥前体/三维内转进气道一体化设计与分析

    航空动力学报,1000-8055,2018.
    李怡庆;周驯黄;朱呈祥;尤延铖
    CSCD核心

  • 乘波前体三维内转进气道气动融合设计

    推进技术,1001-4055,2018.
    李怡庆;施崇广;朱呈祥;尤延铖
    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

  • 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

  • 给定下游边界的超声速流场逆向求解方法

    推进技术,1001-4055,2016-03-29.
    韩伟强;朱呈祥;尤延铖;李怡庆
    CSCD核心 CSCD核心 理工二类核心

  • 横向气流中非牛顿液体射流直接数值模拟

    航空学报,1000-6893,2016-01-31.
    朱呈祥;尤延铖
    CSCD核心 CSCD核心 理工二类核心

  • 引射火箭启动过程的进气道动态特性仿真研究

    气动研究与试验,2097-258X,2024-03-10.
    易理哲;黄玥;王启星;朱呈祥;尤延铖

  • 基于弯曲激波特征线法的两级压缩内收缩流场设计与分析

    气体物理,2096-1642,2022-05-27.
    汤祎麒;施崇广;郑晓刚;朱呈祥;尤延铖

  • 基于弯曲激波特征线法的两级压缩内收缩流场设计与分析

    气体物理,2096-1642,2022-05-27.
    汤祎麒;施崇广;郑晓刚;朱呈祥;尤延铖

  • 高阶弯曲激波理论及其典型应用研究

    空天技术,2097-0714,2022-02-28.
    施崇广;汤祎麒;程剑锐;张涛;朱呈祥;尤延铖

  • 三维内转TBCC进气道模态转换过程流动分析

    第五届空天动力联合会议暨中国航天第三专业信息网第41届技术交流会论文集（第一册）,,2020-09-16.
    蔡泽君;胡占仓;李中龙;张宇超;朱呈祥;尤延铖

  • 三维内转组合进气道模态转换过程流动分析

    中国航天第三专业信息网第四十届技术交流会暨第四届空天动力联合会议论文集——S03冲压及组合推进技术,,2019-08-14.
    胡占仓;朱呈祥;孔凡;尤延铖

  • 重油活塞发动机的燃烧关键技术分析

    小型内燃机与车辆技术,2095-8234,2018.
    朱呈祥;杨日炯

  • 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

  • 剪切稀化流体的撞击破碎数值分析

    2016海峡两岸流体力学研讨会论文摘要集,,2016-09-04.
    尤延铖;朱呈祥

  • 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

  • Numerical investigation on the instability and theprimary breakup of inelastic non-Newtonian liquid jets. (专著). Verlag Dr. Hut, 2014年08月.