Paper Publications

• [1]Zhan DW, Li ZF, Yang JT, Zhu YJ, Yang JM. A contraction channel design for planar shock wave enhancement. Review of Scientific Instruments. 2018, 89(5): 056104. DOI: 10.1063/1.5025223.2021,
• [2]Li ZF, Huang R, Li YM, Yang JM. Sliding-plug approach for inlet self-starting ability test in shock tunnel. AIAA Journal, 2018, 56(9):3785-3790. DOI: 10.2514/1.J056723.2021,
• [3]Huang R, Li ZF, Yang JM. Engineering Prediction of Fluctuating Pressure over Incident Shock/Turbulent Boundary-Layer Interactions. AIAA Journal, 2019, 57(5):2209-2213. DOI: 10.2514/1.J057903.2021,
• [4]Li ZF, Zhang ZY, Wang J, Yang JM. Pressure-Heat Flux Correlations for Shock Interactions on V-Shaped Blunt Leading Edges. AIAA Journal, 2019, 57(10):4588-4592. DOI: 10.2514/1.J058538.2021,
• [5]Zhang EL, Li ZF, Li YM, Yang JM. Three-dimensional shock interactions and vortices on a V-shaped blunt leading edge. Physics of Fluids, 2019, 31(8): 086102. DOI: 10.1063/1.5101031.2021,
• [6]Zhang ZY, Li ZF, Huang R, Yang JM. Experimental investigation of shock oscillations on V-shaped blunt leading edges. Physics of Fluids, 2019, 31(2): 026110. DOI: 10.1063/1.5084184.2021,
• [7]Wang DX, Li ZF, Zhang ZY, Liu NS, Yang JM, Lu XY. Unsteady shock interactions on V-shaped blunt leading edges. Physics of Fluids, 2018, 30(11): 116104. DOI: 10.1063/1.5051012.2021,
• [8]Wang J, Li ZF, Zhang ZY, Yang JM. Shock Interactions on V-Shaped Blunt Leading Edges with Various Conic Crotches. AIAA Journal, 2020, 58(3):1407-1411. DOI: 10.2514/1.J059067.2021,
• [9]Li YM, Li ZF, Yang JM. Tomography-like flow visualization of a hypersonic inward-turning inlet. Chinese Journal of Aeronautics, 2021, 34(1): 44-49. DOI: 10.1016/j.cja.2020.10.012.2021,
• [10]Xiao FS, Li ZF, Zhang ZY, Zhu YJ, Yang JM. Hypersonic Shock Wave Interactions on a V-Shaped Blunt Leading Edge. AIAA Journal, 2018, 56(1):356-367. DOI: 10.2514/1.J055915.2021,