学者信息

黄玥 (Yue Huang)

航空航天学院

国家级重点青年人才; 厦门大学“南强青年拔尖人才”A类; 福建省高层次B类人才; 厦门市高层次B类人才。

2014年度南京航空航天大学优秀博士论文 2019年福建省科技进步一等奖(排名第五) 2020年教育部技术发明一等奖(排名第三)

中国航发科技委外部委员、中国航发产学研联合体副秘书长;担任中国工程热物理学会爆震与新型推进动力委员会委员,中国航空学会动力分会燃烧与传热委员会委员,三网爆震专业委员会委员,担任中国空气动力学燃烧空气动力专委会委员。

《推进技术》《空气动力学学报》《实验流体力学》《空气动力学进展(英文)》、《航空动力学报》等多个期刊青年编委

合作者

已发表成果:

WOK 论文 51 篇;中文核心 17 篇;其它论文 6 篇;专利发明 7 个;

  • Numerical simulation of mixing characteristic of rear variable area bypass injector with lobed structure

    Hangkong Dongli Xuebao/Journal of Aerospace Power,1000-8055,2024-08.
    Liu, Runfu (1); Huang, Yue (1); Li, Zhenyao (1); Zhang, Huiliu (1); You, Yancheng (1)
    EI:20243416919061   10.13224/j.cnki.jasp.20220594
    收录情况:EI
  • Numerical simulations and theoretical analysis of the forward shock wave in a non-premixed air-breathing rotating detonation combustor

    Physics of Fluids,1070-6631,2024-06-01.
    Gao, Sijia; Peng, Han; Huang, Yue; Sun, Zhipeng; You, Yancheng
    WOS:001239083900009   EI:20242316215858   10.1063/5.0206965
    收录情况:SCIE、EI
  • Two-dimensional temperature field inversion of turbine blade based on physics-informed neural networks

    Physics of Fluids,1070-6631,2024-03-01.
    Mai, Jieai; Li, Yang; Long, Lian; Huang, Yue; Zhang, Huiliu; You, Yancheng
    WOS:001180556400019   EI:20241115737374   10.1063/5.0190429
    收录情况:SCIE、EI
  • Outlet boundary condition and mean temperature gradient effects on the minimum acoustics disturbances energy in triggering nonlinear thermoacoustic instability

    Physics of Fluids,1070-6631,2024-03-01.
    Zhao, Xinyu; Zhao, Dan; Shelton, Cody M.; Wang, Bing; Dong, Xu; Li, Junwei; Huang, Yue
    WOS:001184169800009   EI:20241215781347   10.1063/5.0191982
    收录情况:SCIE、EI
  • Numerical study of steady flow characteristics of a rear variable-area bypass injector with alternating area regulator

    Chinese Journal of Aeronautics,1000-9361,2024.
    Liu, Runfu; Li, Zhenyao; Zhang, Huiliu; Wang, Qixing; Huang, Yue; You, Yancheng
    WOS:001241702200002   EI:20241515900044   10.1016/j.cja.2024.01.027
    收录情况:SCIE、EI
  • Experimental and numerical study of combustion characteristics of ammonia-hydrogen-air swirling flame with/without secondary air injection

    Chinese Journal of Aeronautics,1000-9361,2024.
    Liu, Chunyu; Gao, Chenhu; Huang, Yue; Jin, Hua; Zhao, Dan; Xu, Wenjiang; You, Yancheng
    WOS:001224780700001   EI:20241015696870   10.1016/j.cja.2024.01.015
    收录情况:SCIE、EI
  • Numerical investigation of the effects of cooling jets on flow and cooling film characteristics downstream of air-cooled integrated flameholder

    Aerospace Science and Technology,1270-9638,2023-10.
    Chen, Yuqian; Fan, Yuxin; Huang, Yue
    WOS:001050709900001   EI:20233114459682   10.1016/j.ast.2023.108527
    收录情况:SCIE、EI
  • Numerical Study on Effects of Expansion Wave on Wedge-Stabilized Oblique Detonation Wave

    Tuijin Jishu/Journal of Propulsion Technology,1001-4055,2023-10.
    Li, Zhi-Min (1); Peng, Han (2); Luan, Zhen-Ye (1); Long, Zhen-Yu (1); Huang, Yue (1); You, Yan-Chen...
    EI:20242016093641   10.13675/j.cnki.tjjs.2211055
    收录情况: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
  • Formation and Evolution of Cellular Structures in Wedge-Induced Oblique Detonations

    International Journal of Aerospace Engineering,1687-5966,2023.
    Yu, Chengxuan; Luan, Zhenye; Jin, Hua; Huang, Yue; You, Yancheng
    WOS:000965261000001   EI:20231613942429   10.1155/2023/7764076
    收录情况:SCIE、EI
  • Pressurization Characteristics and Flow Field Analysis of Methane/Oxygen Rotating Detonation Combustor at High Temperature and High Pressure Inlets

    Tuijin Jishu/Journal of Propulsion Technology,1001-4055,2022-11.
    Sun, Zhi-Peng (1); Huang, Yue (1); Luan, Zhen-Ye (1); Gao, Si-Jia (1); You, Yan-Cheng (1)
    EI:20232114135546   10.13675/j.cnki.tjjs.210751
    收录情况:EI
  • Flow characterization during the flame acceleration and transition-to-detonation process with solid obstacles and fluid jets

    SHOCK WAVES,0938-1287,2022-11.
    Luan, Z.; Huang, Y.; Deiterding, R.; Peng, H.; You, Y.
    WOS:000878942300001   10.1007/s00193-022-01100-7
    收录情况:SCIE
  • Formation of multiple detonation waves in rotating detonation engines with inhomogeneous methane/oxygen mixtures under different equivalence ratios

    Combustion and Flame,0010-2180,2022-07.
    Luan, Zhenye; Huang, Yue; Gao, Sijia; You, Yancheng
    WOS:000794039500006   EI:20221211810793   10.1016/j.combustflame.2022.112091
    收录情况:SCIE、EI
  • On the evolutions of triple point structure in wedge-stabilized oblique detonations

    PHYSICS OF FLUIDS,1070-6631,2022-06.
    Luan, Zhenye; Huang, Yue; Deiterding, Ralf; You, Yancheng
    WOS:000816084400002   EI:20222812355067   10.1063/5.0090975
    收录情况:SCIE、EI
  • Numerical investigation of non-premixed H2-Air rotating detonation combustor with different equivalence ratios

    Journal of Physics: Conference Series,1742-6588,2022-05-17.
    Jiang, Hanyu (1); Huang, Yue (1)
    EI:20222312190987   10.1088/1742-6596/2235/1/012011
    收录情况:EI
  • Improved delayed detached eddy simulation of supersonic combustion fueled by liquid kerosene

    Fuel,0016-2361,2022-04-01.
    Shen, Wubingyi; Huang, Yue; Yao, Wei; Liu, Hedong; You, Yancheng
    WOS:000743151900003   EI:20220111423979   10.1016/j.fuel.2021.123031
    收录情况:SCIE、EI
  • Thermodynamic Process and Performance Analysis of Inter-Stage Turbine Rotating Detonation Turboshaft Engine

    Tuijin Jishu/Journal of Propulsion Technology,1001-4055,2022-04.
    Zhao, Ting (1); Zhu, Jian-Feng (1); Huang, Xing (2); Huang, Yue (1); You, Yan-Cheng (1)
    EI:20221411925275   10.13675/j.cnki.tjjs.200894
    收录情况:EI
  • Study on the flow characteristics in the non-detonation reaction zones of wedge-induced oblique detonation transitions

    AEROSPACE SCIENCE AND TECHNOLOGY,1270-9638,2022-01.
    Huang, Yue; Luan, Zhenye; Li, Zhimin; Ji, Hua; You, Yancheng
    WOS:000774060000005   10.1016/j.ast.2021.107282
    收录情况:SCIE
  • Three-dimensional simulation of a rotating detonation engine in ammonia/hydrogen mixtures and oxygen-enriched air

    International Journal of Hydrogen Energy,0360-3199,2022.
    Sun, Zhipeng; Huang, Yue; Luan, Zhenye; Gao, Sijia; You, Yancheng
    WOS:000962923900001   EI:20224813193468   10.1016/j.ijhydene.2022.11.029
    收录情况:SCIE、EI
  • Modeling of spontaneous Raman scattering for detonation wave imaging

    Physics of Fluids,1070-6631,2021-12-01.
    Tan, Yaqin; Mevel, Remy; Huang, Yue
    WOS:000745660700004   EI:20220211455355   10.1063/5.0076571
    收录情况:SCIE、EI
  • NOx emission and energy conversion efficiency studies on ammonia-powered micro-combustor with ring-shaped ribs in fuel-rich combustion

    JOURNAL OF CLEANER PRODUCTION,0959-6526,2021-10-20.
    Ni, Siliang; Zhao, Dan; You, Yancheng; Huang, Yue; Wang, Bin; Su, Yunpeng
    WOS:000721711900006   EI:20213610874501   10.1016/j.jclepro.2021.128901
    收录情况:SCIE、EI
  • Shock dynamics and expansion characteristics of an aerospike nozzle and its interaction with the rotating detonation combustor

    Aerospace Science and Technology,1270-9638,2021-10.
    Huang, Yue; Xia, Hanqing; Chen, Xiaonan; Luan, Zhenye; You, Yancheng
    WOS:000705191600015   EI:20213110696407   10.1016/j.ast.2021.106969
    收录情况:SCIE、EI
  • Mixing and transient combustion processes of scramjet combustor with transverse injector and hypermixer

    Case Studies in Thermal Engineering,2214-157X,2021-08.
    Shen, Wubingyi; Huang, Yue; Liu, Zongyang; You, Yancheng
    WOS:000672605600005   EI:20212410481419   10.1016/j.csite.2021.101104
    收录情况:SCIE、EI
  • Numerical Investigation on Unsteady Flow of Nozzle in Rotating Detonation Engine

    Tuijin Jishu/Journal of Propulsion Technology,1001-4055,2021-06.
    Xia, Han-Qing (1); Huang, Yue (1); Zhang, Yi-Ning (2); You, Yan-Cheng (1); Li, Dong (2); Luan, Zhen...
    EI:20212510530528   10.13675/j.cnki.tjjs.190721
    收录情况:EI
  • 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
    收录情况: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
    收录情况:EI
  • Effects of wall cooling with microchannels on swirl combustor performance

    Aerospace Science and Technology,1270-9638,2020-11.
    Huang, Yue; Feng, Xinchi; Lin, Zhiwei; You, Yancheng
    WOS:000579863200096   EI:20203709171299   10.1016/j.ast.2020.106160
    收录情况: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; Zhao, Dan; Li, Weixuan; Wang, Zhiyu; Huang, Yue; You, Yancheng; Becker, Sid
    WOS:000569411900002   EI:20202708903898   10.1016/j.paerosci.2020.100620
    收录情况:SCIE、EI
  • Characteristics of reaction zone in a dual-mode scramjet combustor during mode transitions

    Aerospace Science and Technology,1270-9638,2020-04.
    Shen, Wubingyi; Huang, Yue; You, Yancheng; Yi, Lizhe
    WOS:000519335500050   EI:20200708184634   10.1016/j.ast.2020.105779
    收录情况: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
    收录情况: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
    收录情况: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; Huang, Yue; Deiterding, Ralf; You, Yancheng; Luan, Zhenye
    WOS:000657142700003   EI:20195107853099   10.1080/00102202.2019.1700236
    收录情况:SCIE、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
    收录情况: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
    收录情况: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
    收录情况: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
    收录情况: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
    收录情况: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
    收录情况: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   EI:20170303256021   10.3390/en10010048
    收录情况:SCIE、EI
  • 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
    收录情况: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  
    收录情况: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  
    收录情况: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
    收录情况: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
    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
  • 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
    收录情况: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
    收录情况: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  
    收录情况: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
    收录情况: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
    收录情况: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
    收录情况:EI、CPCI-S
  • 组合火焰稳定器横向喷射高温燃油液滴分布特性实验研究

    推进技术,1001-4055,2024-05-29.
    翟文辉;范育新;陈玉乾;黄玥
    CSCD核心库
  • 基于域对抗神经网络的双模态燃烧室跨构型燃烧模态识别

    推进技术,1001-4055,2024-05-06.
    宋婷;刘和东;黄玥;陈玉乾;尤延铖
    CSCD核心库
  • 膨胀波对斜劈稳定斜爆震波特性影响的数值研究

    推进技术,1001-4055,2023-06-02.
    李志敏;彭瀚;栾振业;龙震宇;黄玥;尤延铖
    CSCD核心库
  • 膨胀波对斜劈稳定斜爆震波特性影响的数值研究

    推进技术,1001-4055,2023-06-02.
    李志敏;彭瀚;栾振业;龙震宇;黄玥;尤延铖
    CSCD核心库
  • 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
  • 高温高压进口下甲烷/氧气旋转爆震燃烧室增压特性与流场分析

    推进技术,1001-4055,2022-04-13.
    孙志鹏;黄玥;栾振业;高思佳;尤延铖
    CSCD核心
  • 高温高压进口下甲烷/氧气旋转爆震燃烧室增压特性与流场分析

    推进技术,1001-4055,2022-04-13.
    孙志鹏;黄玥;栾振业;高思佳;尤延铖
    CSCD核心
  • 级间旋转爆震涡轴发动机热力过程及性能分析

    推进技术,1001-4055,2021-07-14.
    赵廷;朱剑锋;黄兴;黄玥;尤延铖
    CSCD核心
  • 圆盘旋转爆震燃烧室中爆震波传播模态

    推进技术,1001-4055,2020-12-04.
    沈吴冰懿;黄玥;尤延铖;黄鸿涛
    CSCD核心
  • 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
    CSCD核心
  • 旋转爆震发动机喷管非定常流动特性的数值模拟研究

    推进技术,1001-4055,2020-03-24.
    夏寒青;黄玥;张义宁;尤延铖;李冬;栾振业
    CSCD核心
  • 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 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
  • 空气进气温度对空桶型燃烧室旋转爆震起爆及传播特性影响实验研究

    推进技术,1001-4055,2025-01-17.
    宋安家;黄玥;彭瀚;孙志鹏
  • 旋转导向钻井系统三肋流道转换器设计研究

    石油矿场机械,1001-3482,2024-11-25.
    杨恒灿;张玉霖;林颢屿;菅志军;鲍东升;黄玥
  • 引射火箭冲压发动机下限及模态转换稳定性研究

    航空动力,2096-5702,2024-06-18.
    黄玥;刘和东
  • 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
  • 跨音速轴向压气机叶尖间隙流动模拟的湍流模型适用性分析

    第六届空天动力联合会议暨中国航天第三专业信息网第四十二届技术交流会暨2021航空发动机技术发展高层论坛论文集(第一册),,2021-12-14.
    蒋撼宇;黄玥;尤延铖
  • Ma1.8时BUMP进气道激波振荡特性的脱体涡模拟

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