Researcher's Profile

Huang Yue(黄玥)

School of Aerospace Engineering

南京航空航天大学 2014年度优秀博士论文


Research Area:


  • 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, Xiaolei(4)
    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)
    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)
    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)
    Included in : EI
  • Experimental and numerical study of thermal enhancement in reentrant copper microchannels

    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
  • 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.
  • 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.
    CSCD核心 理工二类核心
  • On the operational parameters effects on two-phase pressure drop characteristics of reentrant copper microchannels

    Deng, Daxiang; Huang, Qingsong; Xie, Yanlin; Zhou, Wei; Huang, Xiang; Huang, Yue