Yue Huang
Professor
▶Liu H, Chen Y, Shan X, Zhu J, Fan Y, Huang Y, et al. (2025). Effects of the cooling jets on the flame characteristics and wall temperature of air-cooled wall-strut flameholders, Aerospace Science and Technology, 157: 109781.
▶Sun Z, Peng H, Huang Y*, et al. (2024). Propagation and stabilization properties of rotating detonation waves in a hollow combustion chamber with heated air inflow, Physics of Fluids, 36: 106143.
▶Gao S, Peng H, Huang Y*, et al. (2024). Numerical simulations and theoretical analysis of the forward shock wave in a non-premixed air-breathing rotating detonation combustor, Physics of Fluids, 36, 066101.
▶Liu R, Li Z, Zhang H, Wang Q, Huang Y*, et al. (2024). Numerical study of steady flow characteristics of a rear variable-area bypass injector with alternating area regulator, Chinese Journal of Aeronautics, 37(5), 180-198.
▶Liu C, Gao C, Huang Y*, et al. (2024). Experimental and numerical study of combustion characteristics of ammonia–hydrogen–air swirling flame with/without secondary air injection, Chinese Journal of Aeronautics, 37(4): 243-255.
▶Ma M, Luo S, Peng H, Cai J, Xu W, Huang Y, et al. (2024). Experimental study of flame dynamics and NOx emission characteristics in a NH₃-H₂ blended non-premixed swirl combustor, International Journal of Hydrogen Energy, 110: 324-335.
▶Mai J, Li Y, Long L, Huang Y*, et al. (2024). Two-dimensional temperature field inversion of turbine blade based on physics-informed neural networks, Physics of Fluids, 36: 037114.
▶Sun Z, Huang Y*, Luan Z, et al. (2023). Three-dimensional simulation of a rotating detonation engine in ammonia/hydrogen mixtures and oxygen-enriched air, International Journal of Hydrogen Energy, 48:4891-4905.
▶Luan Z, Huang Y*, Gao S, et al. (2022). Formation of multiple detonation waves in rotating detonation engines with inhomogeneous methane/oxygen mixtures under different equivalence ratios, Combustion and Flame, 112091.
▶Luan Z, Huang Y*, Deiterding R et al. (2022). On the evolutions of triple points structure in wedge-stabilized oblique detonations, Physics of Fluids, 34: 067118.
▶Shen W, Huang Y*; Yao W, et al. (2022). Improved delayed detached eddy simulation of supersonic combustion fueled by liquid kerosene, Fuel, 313:123031.
▶Huang Y*, Xia H, Chen X, et al. (2021). Shock dynamics and expansion characteristics of an aerospike nozzle and its interaction with the rotating detonation, Aerospace Science and Technology , 117: 106969.
▶Peng H, Huang Y*, Deiterding R, et al. (2018). Effects of jet in crossflow on flame acceleration and deflagration to detonation transition in methane-oxygen mixture, Combustion and Flame, 198: 69-80.
▶ 宋婷，刘和东，黄玥，陈玉乾，尤延铖. 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，2025,46(2):129-144.
▶刘润富，黄玥，李臻曜，张慧骝，尤延铖. 波瓣结构后可变面积涵道引射器掺混特性. 航空动力学报，2024,39 (8), 20220594.
▶李志敏，彭瀚，栾振业，龙震宇，黄玥, 尤延铖.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，2023, 44 (10), 131-139.
▶Luan Z, Huang Y*, Deiterding R, et al. (2022). Flow characterization during the flame acceleration and transition-to-detonation process with solid obstacles and fluid jets, Shock Waves, 32: 617–632.
▶Huang Y, Luan Z, Li Z, et al. (2022). Study on the flow characteristics in the non-detonation reaction zones of wedge-induced oblique detonation transitions, Aerospace Science and Technology, 120: 107282.
▶林志伟，黄玥*，邢菲，沈倩，李爱成. 壁面微通道冷却对旋流燃烧室性能影响实验研究.航空动力学报，2019, 34 (2) :376-386.
▶ 彭瀚，黄玥*，刘晨，邢菲，栾振业. 横向射流影响缓燃向爆震转捩过程的试验研究. 航空学报，2018,39 (2): 121412.
▶ 彭瀚，黄玥*，邢菲，刘晨，林志伟. 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，2017 ,32(1):60-65.
▶易理哲，黄玥*，王启星，朱呈祥，尤延铖. 引射火箭启动过程的进气道动态特性仿真研究. 气动研究与实验，2021, 33(03): 24-30 .
▶尹泽勇，尤延铖，朱呈祥，朱剑锋，吴了泥，黄玥. 面向高超民机的多通道双涡轮引射冲压组合动力. 航空学报，2023，44(2):627181 .
▶Jiang H, Huang Y*. (2022). Numerical investigation of non-premixed H2-Air rotating detonation combustor with different equivalence ratios. Journal of Physics, 2235(2022): 012011.
▶Liu C, Huang Y*,Yang W, et al. (2017) Study on effects of fluidic obstacles on flame acceleration and deflagration-to-detonation transition. AIAA-2017-2261.
▶Tan Y, Mével R; Huang Y (2021) Modeling of spontaneous Raman scattering for detonation wave imaging. Physics of Fluids, 33:126115.
▶Ni S, Zhao, D, You, Y, Huang Y, et al. (2021) NOx emission and energy conversion efficiency studies on ammonia-powered micro-combustor with ring-shaped ribs in fuel-rich combustion. Journal of Cleaner Production, 320: 128901.
▶Xing F, Arvind K, Huang Y, et al. (2017) Flameless combustion with liquid fuel: A review focusing on fundamentals and gas turbine application. Applied Energy ,193: 28-51.
▶Wang B, Zhao D, Li W, Wang Z, Huang Y; et al. (2020) Current technologies and challenges of applying fuel cell hybrid propulsion systems in unmanned aerial vehicles, Progress in Aerospace Sciences , 116: 100620.
▶Deng D, Xie Y, Chen L, Pi Gg, Huang Y. (2019) Experimental investigation on thermal and combustion performance of a combustor with microchannel cooling, Energy , 181: 954-963.
▶Wan W, Deng D, Huang Q, Zeng T, Huang Y. (2017) Experimental study and optimization of pin fin shapes in flow boiling of micro pin fin heat sinks. Applied Thermal Engineering, 114 : 436-449.
▶刘润富，黄玥，李臻曜，张慧骝，尤延铖. (2024) 波瓣结构后可变面积涵道引射器掺混特性,航空动力学报，39(8): 20220594
