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;
Flow characterization during the flame acceleration and transition-to-detonation process with solid obstacles and fluid jets
Pressurization Characteristics and Flow Field Analysis of Methane/Oxygen Rotating Detonation Combustor at High Temperature and High Pressure Inlets
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
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.