的个人主页 http://shi.buaa.edu.cn/zhangguangyu/zh_CN/index.htm
英文学术论文:
[1] Zhang G, Yang N, Wang Y, Li L, Wang X, Yang D, Lin Y, Sun X. Combustion instabilities of bluff-body stabilized liquid spray flames coupled with pressure oscillations in the fuel line[J]. Combustion and Flame, 2025, 273: 113911.
[2] Dai W, Qin W, Wang X, Zhang G*, Sun X. On the analytical acoustic propagation and mode decomposition method in C-duct[J]. Applied Acoustics, 2025, 235: 110704.
[3] Shen Z, Wang X, Li J, Zhang G, Sun X. Acoustic resonance in annular cascades in the presence of background mean flow[J]. Journal of Fluid Mechanics, 2024, 1006: A7.
[4] Dai W, Wang X, Zhang G*, Sun X. Estimating method for azimuthal thermoacoustic mode in annular combustors[C]//Journal of Physics: Conference Series. IOP Publishing, 2025, 2977(1): 012098.
[5] Shen Z, Wang X, Zhang G*, Sun X. Effects of Radially Variable Sweep Vanes on Rotor–Stator Interaction Noise[J]. Journal of Turbomachinery, 2025, 147(5).
[6] Zhou W, Wang X, Zhang G, Heckl M, Sun X. Three-dimensional interaction of thermoacoustic modes in a circular tube[J]. Journal of Sound and Vibration, 2024: 118899.
[7] Qin L, Wang X, Zhang G*, Sun X. Suppression of Azimuthal Combustion Instability Using Perforated Liner Under Symmetry Breaking[J]. Journal of Propulsion and Power, 2024: 1-13.
[8] Liu C, Wang X, Gao F, Zhang G*, Sun X. Effect of Over-the-Rotor Liner on Fan Flutter Stability[J]. AIAA Journal, 2024: 1-9.
[9] Zhang G, Zhang X, Wang X, Sun X. Modeling analysis of combustion instability in an annular combustor equipped with circumferentially segmented perforated liner[J]. Journal of Sound and Vibration, 2023: 117573.
[10] Dai W, Wang X, Wang X, Zhang G*, Sun X. Acoustic scattering mechanism and noise attenuation of circumferentially non-uniform liner with spectral-wave guide method[J]. Chinese Journal of Aeronautics, 2023, 36(9): 63-78.
[11] Shen Z, Wang X*, Sun Y, Zhang G, Sun X. Three-dimensional effects of cascade perforations on rotor–stator interaction noise[J]. Journal of Fluid Mechanics, 2022, 952: A7.
[12] Chen Z X*, Swaminathan N, Mazur M, Worth N, Zhang G, Li L. Numerical investigation of azimuthal thermoacoustic instability in a gas turbine model combustor[J]. Fuel, 2023, 339: 127405.
[13] Xu L, Zhang G, Wang G, Feng Z, Tian X, Li L*, Qi F. Effects of acoustic liner on thermoacoustic instabilities in a premixed swirl combustor[J]. Aerospace Science and Technology, 2021, 118: 107070.
[14] Qin L, Wang X*, Zhang G, Sun X. Effect of nonlinear flame response on the design of perforated liners in suppression of combustion instability[J]. Journal of Sound and Vibration, 2021, 511: 116314.
[15] Zhang G, Wang X*, Li L, Sun X. Effects of perforated liners on controlling combustion instabilities in annular combustors[J]. AIAA Journal, 2020, 58(7): 3100-3114.
[16] Zhang G, Wang X*, Li L, Sun X. Control of thermoacoustic instability with a drum-like silencer[J]. Journal of Sound and Vibration, 2017, 406: 253-276.
中文学术论文:
[1] 孙晓峰, 张光宇 *, 王晓宇, 李磊, 邓向阳, 程荣辉. 航空发动机燃烧不稳定性预测及控制研究进展(“航空发动机非定常流固热声耦合”专栏)[J]. 航空学报, doi: 10.7527/S1000-6893.2023.28733.
[2] 张琦祥, 任立磊, 李威, 秦维锐, 张光宇*, 王晓宇, 孙晓峰. 穿孔板声衬降噪特性的理论与实验研究, 中国科学: 技术科学, 2024, ISSN 1674-7259, https://doi.org/10.1360/SST-2024-0164.
[3] 刘传洋, 王晓宇, 张光宇*, 孙晓峰. 大厚度穿孔板声阻抗试验研究,航空学报,1-14[2025-04-07].http://kns.cnki.net/kcms/detail/11.1929.V.20250217.1127.002.html.