›中国工程物理研究院（装备研发）:大口径发射试验系统（子课题），300万元，在研，主持

›国家自然科学基金委-青年科学基金项目:前台阶对高超声速圆锥边界层转捩的影响机制及转捩控制方法(12402279),徐席旺,开始日期:2025-01-01,立项时间:2024-08-23,结项时间:2027-12-31.

›国家重点研发计划:激波/湍流边界层干扰机理的实验研究(2019YFA0405301),开始日期:2019-11-01,结项时间:2024-10-31.

›国家自然科学基金面上项目:高超声速流向角区激波反射与流动分离机理研究(12472242),开始日期:2025-01-01,结项时间:2028-12-31.

›Xiwang Xu (徐席旺), Zihao Ye (叶子豪), Shihe Yi (易仕和), Yufa Hu (胡玉发), Lican Wang (王李璨).Experimental investigation on the hypersonic boundary layer transition induced by side-by-side cylinders.Physics of Fluids, 2026, 38 (2)

›Yufa Hu, Xiaolin Liu, Shihe Yi, Chenyang Han, Siyuan Ju, Xiwang Xu.Shear layer flow behavior between low-speed wall-seeping helium gas film and hypersonic freestream over a cone.Chinese Journal of Aeronautics, 2025

›Zihao Ye, Xiwang Xu, Shihe Yi, Jiarui Liu, Zhen Zhang, Ruitong Zeng.Influences of herringbone riblets on shock-wave/turbulent boundary layer interactions in supersonic compression-ramp flow.Physics of Fluids, 2025, 37 (8) : 1-16.

›Xiwang Xu, Shihe Yi, Yufa Hu, Zihao Ye, Lin He.Influences of steps on hypersonic boundary layer instability over a cone at small angle of attack[J].Physics of Fluids, 2025, 37 (6)

›Xiwang Xu, Zihao Ye, Shihe Yi.Experimental study on influences of steps on hypersonic boundary layer transition at different angles-of-attack.Physics of Fluids, 2024, 36: 084109.

›胡玉发, 易仕和, 刘小林, 徐席旺, 张震, 张臻.壁面渗透气膜工质对圆锥高超声速边界层稳定性的影响.物理学报, 2024, 73 (12) : 150-163.

›Yufa Hu, Shihe Yi, Xiaolin Liu, Xiwang Xu.Experimental investigation on the effect of wall-seeping gas film on downstream second-mode waves in hypersonic boundary layer.Aerospace Science and Technology, 2024, 146: 108951.

›Haoxi Xiong, Xiwang Xu, Shihe Yi.Experimental Investigation of the Hypersonic Boundary-Layer Transition Induced by the Wall-Mounted Cylinder.Journal of Thermophysics and Heat Transfer, 2023, 37 (4) : 740-749.

›Pengcheng Quan, Gang Wang, Xiwang Xu.Experimental investigation on effects of herringbone riblets on shock wave/boundary layer interactions of a compression ramp at Mach 3.Physics of Fluids, 2023, 35 (6) : 066131.

›Xiwang Xu, Shihe Yi, Pengcheng Quan.Experimental study on the hypersonic boundary layer transition induced by tandem cylinders[J].Experimental Thermal and Fluid Science, 2023, 145: 110901.

›Zihao Xia, Haolin Ding, Xiwang Xu.Experimental study on the aero-optical effects of a supersonic mixing layer controlled by the ramp vortex generator array.Applied Optics, 2022, 61 (24)

›Xiwang Xu, Shihe Yi, Junhao Han.Effects of steps on the hypersonic boundary layer transition over a cone at 10° angle-of-attack.Physics of Fluids, 2022, 34 (3) : 034114.

›Xiwang Xu, Shihe Yi, Pengcheng Quan.Delaying hypersonic boundary layer transition using forward-facing step arrays: An experimental work[J].Physics of Fluids, 2022, 34 (6) : 065128.

›Zihao Xia, Haolin Ding, Xiwang Xu.Influence of RVGA’s height on suppressing the aero-optical effects induced by a supersonic mixing layer.Applied Optics, 2022, 61 (35)

›徐席旺, 易仕和, 张锋.高超声速圆锥边界层转捩实验研究.气体物理, 2022, 7 (3) : 45-59.

›Junhao Han, Lin He, Xiwang Xu.Experimental investigation of a roughness element wake on a hypersonic flat plate.Aerospace, 2022, 9 (10) : 574.

›Haoxi Xiong, Xiwang Xu, Shihe Yi, Haolin Ding.3D ray tracing methods across inhomogeneous refractive indices using a transmission equation.Optical Engineering, 2022, 6 (9) : 095101.

›Xiwang Xu, Shihe Yi, Junhao Han.Experimental investigation of the hypersonic boundary layer transition on a sharp cone under different angles-of-attack.32nd Congress of the International Council of the Aeronautical Sciences, 2021

›Zhen Zhang, Yuan Zheng, Xiwang Xu.The Effect of Mixing Chamber Configuration and Submersion Depth on Centrifugal Aerator Performance.Sustainability, 2021

›Feng Zhang, Shihe Yi, Xiwang Xu.A swept fin-induced flow field with different height mounting gaps.Chinese Journal of Aeronautics, 2021, 34 (1) : 148-162.

›Xiwang Xu, Shihe Yi, Feng Zhang.Influences of steps on the hypersonic boundary-layer transition on a cone.AIAA Journal, 2020, 59: 439-446.

›易仕和, 刘小林, 陆小革, 牛海波, 徐席旺.NPLS技术在高超声速边界层转捩研究中的应用.空气动力学学报, 2020, 38 (2) : 348-354.

›Feng Zhang, Shihe Yi, Xiwang Xu.Flow Structure and Heat Flux Distribution of a Backswept Fin Induced Flow Field at M=6.Fluid Dynamics, 2020, 55 (5) : 670-680.

›徐席旺, 易仕和, 张锋.带轴对称台阶的圆锥高超声速边界层转捩试验.宇航学报, 2019, 40 (8) : 908-917.

›Xiaolin Liu, Shihe Yi, Xiwang Xu.Experimental study of second-mode wave on a flared cone at Mach 6.Physics of Fluids, 2019, 31: 074108.

›Qi Mi, Shihe Yi, Xinhai Zhao, Dundian Gang, Xiwang Xu.Effects of Backward-Facing Step Shape on Hypersonic Flow Characteristics.Journal of Thermophysics and Heat Transfer, 2019, 31 (7) : 074108.

›中国空气动力学会科学技术一等奖（发明奖）|2023