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
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
Numerical simulations and theoretical analysis of the forward shock wave in a non-premixed air-breathing rotating detonation combustor
Two-dimensional temperature field inversion of turbine blade based on physics-informed neural networks
Outlet boundary condition and mean temperature gradient effects on the minimum acoustics disturbances energy in triggering nonlinear thermoacoustic instability
Numerical study of steady flow characteristics of a rear variable-area bypass injector with alternating area regulator
Experimental and numerical study of combustion characteristics of ammonia-hydrogen-air swirling flame with/without secondary air injection
Numerical investigation of the effects of cooling jets on flow and cooling film characteristics downstream of air-cooled integrated flameholder
Numerical Study on Effects of Expansion Wave on Wedge-Stabilized Oblique Detonation Wave
Multi-ducted twin-turbines ejector-ramjet/scramjet combined cycle engine for hypersonic civil vehicles
Formation and Evolution of Cellular Structures in Wedge-Induced Oblique Detonations
Pressurization Characteristics and Flow Field Analysis of Methane/Oxygen Rotating Detonation Combustor at High Temperature and High Pressure Inlets
Flow characterization during the flame acceleration and transition-to-detonation process with solid obstacles and fluid jets
Formation of multiple detonation waves in rotating detonation engines with inhomogeneous methane/oxygen mixtures under different equivalence ratios
On the evolutions of triple point structure in wedge-stabilized oblique detonations
Numerical investigation of non-premixed H2-Air rotating detonation combustor with different equivalence ratios
Improved delayed detached eddy simulation of supersonic combustion fueled by liquid kerosene
Thermodynamic Process and Performance Analysis of Inter-Stage Turbine Rotating Detonation Turboshaft Engine
Study on the flow characteristics in the non-detonation reaction zones of wedge-induced oblique detonation transitions
Three-dimensional simulation of a rotating detonation engine in ammonia/hydrogen mixtures and oxygen-enriched air
Modeling of spontaneous Raman scattering for detonation wave imaging
NOx emission and energy conversion efficiency studies on ammonia-powered micro-combustor with ring-shaped ribs in fuel-rich combustion
Shock dynamics and expansion characteristics of an aerospike nozzle and its interaction with the rotating detonation combustor
Mixing and transient combustion processes of scramjet combustor with transverse injector and hypermixer
Numerical Investigation on Unsteady Flow of Nozzle in Rotating Detonation Engine
Propagation Mode of Detonation Wave in a Plane-Radial Rotating Detonation Combustion Chamber
Interaction Between Detonation and Non-Premixed Fuel Jets
Effects of wall cooling with microchannels on swirl combustor performance
Current technologies and challenges of applying fuel cell hybrid propulsion systems in unmanned aerial vehicles
Characteristics of reaction zone in a dual-mode scramjet combustor during mode transitions
Experimental investigation on thermal and combustion performance of a combustor with microchannel cooling
Experiment on effects of wall cooling with microchannels on performances of swirl combustor
Effects of Transverse Jet Parameters on Flame Propagation and Detonation Transition in Hydrogen-Oxygen-Argon Mixture
Effects of jet in crossflow on flame acceleration and deflagration to detonation transition in methane-oxygen mixture
Experimental study of effects of fluidic obstacle parameters on deflagration-to-detonation transition
Vehicle Type Recognition in Surveillance Images From Labeled Web-Nature Data Using Deep Transfer Learning
Experimental study and optimization of pin fin shapes in flow boiling of micro pin fin heat sinks
Performance of ultra-compact inter-turbine burner with different inlet mass flow splits
Numerical investigation on shock train control and applications in a scramjet engine
The Influence of Acoustic Field Induced by HRT on Oscillation Behavior of a Single Droplet
Flameless combustion with liquid fuel: A review focusing on fundamentals and gas turbine application
Numerical analysis of hyshot scramjet model with different throat heights
Study on effects of fluidic obstacle on flame acceleration and deflagration-to-detonation transition
A parametrical study of the breakup and atomization process of two impinging liquid jets
Aeroacoustic and flow field features of ultrasonic atomizer based on Hartmann resonance tube
Effects of incoming boundary layer on injection characteristics of a scramjet combustor
The Brief Introduction of Different Laser Diagnostics Methods Used in Aeroengine Combustion Research
On the operational parameters effects on two-phase pressure drop characteristics of reentrant copper microchannels
Numerical investigation on two streamline-traced busemann inlet-isolators
Experimental and numerical study of thermal enhancement in reentrant copper microchannels
Chemical non-equilibrium flow analysis of H2 fueled scramjet nozzle
Study of the Dump Diffuser Optimization for Gas Turbine Combustors
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.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.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.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.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.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.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.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.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.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.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.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.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.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.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.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.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.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.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.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.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.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.