Researcher's Profile

Yue Huang(黄玥)

School of Aerospace Engineering

南京航空航天大学 2014年度优秀博士论文

中国工程热物理学会爆震与新型推进动力委员会委员

CONTRIBUTOR

已发表成果:

WOK 论文 27 篇;中文核心 4 篇;其它论文 2 篇;专利发明 7 个;

  • Propagation Mode of Detonation Wave in a Plane-Radial Rotating Detonation Combustion Chamber

    Tuijin Jishu/Journal of Propulsion Technology,1001-4055,2021-04.
    Shen, Wu-Bing-Yi (1); Huang, Yue (1); You, Yan-Cheng (1); Huang, Hong-Tao (1)
    EI:20211810274040   10.13675/j.cnki.tjjs.200503
    Included in:EI
  • Interaction Between Detonation and Non-Premixed Fuel Jets

    Tuijin Jishu/Journal of Propulsion Technology,1001-4055,2021-04.
    Luan, Zhen-Ye (1); Huang, Yue (1); Liu, Si-Yuan (1); Jiang, Han-Yu (1)
    EI:20211810273971   10.13675/j.cnki.tjjs.200535
    Included in:EI
  • Effects of wall cooling with microchannels on swirl combustor performance

    Aerospace Science and Technology,1270-9638,2020-11.
    Huang, Yue (1); Feng, Xinchi (1); Lin, Zhiwei (1); You, Yancheng (1)
    WOS:000579863200096   EI:20203709171299   10.1016/j.ast.2020.106160
    Included in:SCIE、EI
  • Current technologies and challenges of applying fuel cell hybrid propulsion systems in unmanned aerial vehicles

    Progress in Aerospace Sciences,0376-0421,2020-07.
    Wang, Bin (1, 2); Zhao, Dan (2); Li, Weixuan (2, 3); Wang, Zhiyu (1); Huang, Yue (4); You, Yancheng...
    EI:20202708903898   10.1016/j.paerosci.2020.100620
    Included in:EI
  • Characteristics of reaction zone in a dual-mode scramjet combustor during mode transitions

    Aerospace Science and Technology,1270-9638,2020-04.
    Shen, Wubingyi (1); Huang, Yue (1); You, Yancheng (1); Yi, Lizhe (1)
    WOS:000519335500050   EI:20200708184634   10.1016/j.ast.2020.105779
    Included in:SCIE、EI
  • Experimental investigation on thermal and combustion performance of a combustor with microchannel cooling

    Energy,0360-5442,2019-08-15.
    Deng, Daxiang (1, 2); Xie, Yanlin (2); Chen, Liang (2); Pi, Guang (2); Huang, Yue (3)
    WOS:000476965900078   EI:20192407047238   10.1016/j.energy.2019.06.034
    Included in:SCIE、EI
  • Experiment on effects of wall cooling with microchannels on performances of swirl combustor

    Hangkong Dongli Xuebao/Journal of Aerospace Power,1000-8055,2019-02-01.
    Lin, Zhiwei (1); Huang, Yue (1); Xing, Fei (1); Shen, Qian (1); Li, Aicheng (2)
    EI:20192106951229   10.13224/j.cnki.jasp.2019.02.014
    Included in:EI
  • Effects of Transverse Jet Parameters on Flame Propagation and Detonation Transition in Hydrogen–Oxygen–Argon Mixture

    Combustion Science and Technology,0010-2202,2019.
    Peng, Han (1, 2); Huang, Yue (1); Deiterding, Ralf (2); You, Yancheng (1); Luan, Zhenye (1)
    EI:20195107853099   10.1080/00102202.2019.1700236
    Included in:EI
  • Effects of jet in crossflow on flame acceleration and deflagration to detonation transition in methane-oxygen mixture

    COMBUSTION AND FLAME,0010-2180,2018-12.
    Peng, H; Huang, Y; Deiterding, R; Luan, ZY; Xing, F; You, YC
    WOS:000452581400006   10.1016/j.combustflame.2018.08.023
    Included in:SCIE
  • Experimental study of effects of fluidic obstacle parameters on deflagration-to-detonation transition

    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,1000-6893,2018-02-25.
    Peng, Han (1); Huang, Yue (1); Liu, Chen (1); Xing, Fei (1); Luan, Zhenye (1)
    EI:20182505350770   10.7527/S1000-6893.2017.121412
    Included in:EI
  • Vehicle Type Recognition in Surveillance Images From Labeled Web-Nature Data Using Deep Transfer Learning

    IEEE Transactions on Intelligent Transportation Systems,1524-9050,2017-11-26.
    Wang, Jitian(1); Zheng, Han(1); Huang, Yue(2); Ding, Xinghao(1)
    WOS:000444611400015   EI:20174904503740   10.1109/TITS.2017.2765676
    Included in:SCIE、EI
  • Experimental study and optimization of pin fin shapes in flow boiling of micro pin fin heat sinks

    Applied Thermal Engineering,1359-4311,2017-03-05.
    Wan, Wei(1); Deng, Daxiang(1,2); Huang, Qingsong(1); Zeng, Tao(1); Huang, Yue(3)
    WOS:000395725400040   EI:20165103133351   10.1016/j.applthermaleng.2016.11.182
    Included in:SCIE、EI
  • Performance of ultra-compact inter-turbine burner with different inlet mass flow splits

    Hangkong Dongli Xuebao/Journal of Aerospace Power,1000-8055,2017-01-01.
    Peng, Han(1); Huang, Yue(1); Xing, Fei(1); Liu, Chen(1); Lin, Zhi-Wei(1)
    EI:20171203478258   10.13224/j.cnki.jasp.2017.01.009
    Included in:EI
  • Numerical investigation on shock train control and applications in a scramjet engine

    Aerospace Science and Technology,1270-9638,2017-01-01.
    Xing, Fei(1); Ruan, Can(1); Huang, Yue(1); Fang, Xiaoyuan(1); Yao, Yufeng(2)
    WOS:000392791200016   EI:20164903086440   10.1016/j.ast.2016.11.007
    Included in:SCIE、EI
  • The Influence of Acoustic Field Induced by HRT on Oscillation Behavior of a Single Droplet

    ENERGIES,1996-1073,2017-01.
    Ruan, Can; Xing, Fei; Huang, Yue; Yu, Xinyi; Zhang, Jiacheng; Yao, Yufeng
    WOS:000392422500048   10.3390/en10010048
    Included in:SCIE
  • Flameless combustion with liquid fuel: A review focusing on fundamentals and gas turbine application

    Applied Energy,0306-2619,2017.
    Xing, Fei(1); Kumar, Arvind(2); Huang, Yue(1); Chan, Shining(1); Ruan, Can(1); Gu, Sai(3); Fan, Xia...
    EI:20170803371841   10.1016/j.apenergy.2017.02.010
    Included in:EI
  • Study on effects of fluidic obstacle on flame acceleration and deflagration-to-detonation transition

    21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017,,2017.
    Liu, Chen(1); Huang, Yue(1); Yang, Weizhe(1); Peng, Han(1); Xing, Fei(1); You, Yancheng(1)
    EI:20171603581484  
    Included in:EI
  • Numerical analysis of hyshot scramjet model with different throat heights

    21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017,,2017.
    Xing, Fei(1); Cai, Jiangqian(1); Huang, Yue(1); Yao, Yufeng(2)
    EI:20171603581642  
    Included in:EI
  • A parametrical study of the breakup and atomization process of two impinging liquid jets

    Atomization and Sprays,1044-5110,2017.
    Ruan, Can(1,2); Xing, Fei(1); Huang, Yue(1); Xu, Leilei(2); Lu, Xingcai(2)
    WOS:000426056600002   EI:20181004851534   10.1615/AtomizSpr.2017020941
    Included in:SCIE、EI
  • Aeroacoustic and flow field features of ultrasonic atomizer based on Hartmann resonance tube

    Hangkong Dongli Xuebao/Journal of Aerospace Power,1000-8055,2016-09-01.
    Ruan, Can(1); Huang, Yue(1); Cai, Jiang-Qian(1); Liu, Chen(1); Xing, Fei(1)
    EI:20164202916177   10.13224/j.cnki.jasp.2016.09.008
    Included in: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
    Included in:EI
  • The Brief Introduction of Different Laser Diagnostics Methods Used in Aeroengine Combustion Research

    Journal of Sensors,1687-725X,2016.
    Xing, Fei(1); Huang, Yue(1); Zhao, Mengmeng(2); Zhao, Jian(3)
    WOS:000372974800001   EI:20161002063980   10.1155/2016/2183569
    Included in:SCIE、EI
  • On the operational parameters effects on two-phase pressure drop characteristics of reentrant copper microchannels

    ASME 2016 5th International Conference on Micro/Nanoscale Heat and Mass Transfer, MNHMT 2016,,2016.
    Deng, Daxiang(1,2); Huang, Qingsong(1); Xie, Yanlin(1); Zhou, Wei(1); Huang, Xiang(3); Huang, Yue(1)
    EI:20162102413950   10.1115/MNHMT2016-6514
    Included in:EI
  • Numerical investigation on two streamline-traced busemann inlet-isolators

    54th AIAA Aerospace Sciences Meeting,,2016.
    Xing, Fei(1); Huang, Yue(1); Fang, Xiaoyuan(1); Yao, Yufeng(2)
    EI:20170103223099  
    Included in:EI
  • Experimental and numerical study of thermal enhancement in reentrant copper microchannels

    INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER,0017-9310,2015-12.
    Deng, Daxiang; Wan, Wei; Tang, Yong; Shao, Haoran; Huang, Yue
    WOS:000362130700068   EI:20153501207561   10.1016/j.ijheatmasstransfer.2015.08.025
    Included in:SCIE、EI
  • Chemical non-equilibrium flow analysis of H2 fueled scramjet nozzle

    Case Studies in Thermal Engineering,2214-157X,2015-03-01.
    Huang, Yue(1); Wang, Peiyong(1); Dou, Yang(1); Xing, Fei(1)
    EI:20151700794685   10.1016/j.csite.2015.02.002
    Included in:EI
  • Study of the Dump Diffuser Optimization for Gas Turbine Combustors

    Procedia Engineering,,2015.
    Xu, Leilei(1); Huang, Yue(1); Ruan, Can(1); Peiyong Wang;Fei Xing
    WOS:000384483200104   EI:20162902602100   10.1016/j.proeng.2014.12.608
    Included in:EI、CPCI-S
  • 壁面微通道冷却对旋流燃烧室性能影响实验

    航空动力学报,1000-8055,2019-01-25.
    林志伟;黄玥;邢菲;沈倩;李爱成
    CSCD核心
  • 横向射流影响缓燃向爆震转捩过程的试验研究

    航空学报,1000-6893,2018.
    彭瀚;黄玥;刘晨;邢菲;栾振业
    CSCD核心
  • 入口流量分配对超紧凑级间燃烧室性能的影响

    航空动力学报,1000-8055,2017-01-01.
    彭瀚;黄玥;邢菲;刘晨;林志伟
    CSCD核心
  • 基于Hartmann谐振腔的雾化喷嘴声场流场特性

    航空动力学报,1000-8055,2016-09-20.
    阮灿;黄玥;蔡江千;刘晨;邢菲
    CSCD核心 理工二类核心
  • 圆盘旋转爆震燃烧室中爆震波传播模态

    推进技术,1001-4055,2020/12/4.
    沈吴冰懿; 黄玥; 尤延铖; 黄鸿涛
  • 爆震波与非预混燃料射流相互作用的研究

    推进技术,1001-4055,2020/11/16.
    栾振业; 黄玥; 刘思远; 蒋撼宇