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Author

Haibo Niu

Observed names: H. B. Niu, Hai-Bo Niu, Haibo NIU, Niu Hai-Bo
ORCID: 0000-0002-5122-9302
Observed ORCID: 0000-0002-5122-9302
OpenAlex ID: A5003084031
Experimental investigation of boundary layer transition over a delta wing at Mach number 6
2020 · Haibo NIU, Shihe YI, et al. · Chinese Journal of Aeronautics · 29
A swept fin-induced flow field with different height mounting gaps
2020 · Feng ZHANG, Shihe YI, et al. · Chinese Journal of Aeronautics · 26
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Experimental Study of Crossflow Instability over a Delta Flat Plate at Mach 6
2019 · Haibo Niu, Shihe Yi, et al. · AIAA Journal · 24
Experimental investigation about the second-mode waves in hypersonic boundary layer over a cone at small angle of attack
2020 · Xiaolin Liu, Shihe Yi, et al. · Experimental Thermal and Fluid Science · 21
Experimental investigation of expansion effect on shock wave boundary layer interaction near a compression ramp
2022 · Junjie HUO, Shihe YI, et al. · Chinese Journal of Aeronautics · 17
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Experimental study of hypersonic traveling crossflow instability over a yawed cone
2022 · Haibo Niu, Shihe Yi, et al. · Acta Astronautica · 14
Experimental study on hypersonic crossflow instability over a swept flat plate by flow visualization
2021 · Hai-Bo Niu, Shi-He Yi, et al. · Acta Mechanica Sinica · 14
Experimental investigation of nose-tip bluntness effects on the hypersonic crossflow instability over a cone
2020 · Haibo Niu, Shihe Yi, et al. · International Journal of Heat and Fluid Flow · 13
Effects of sweep angles on turbulent separation behaviors induced by blunt fin
2021 · Dundian GANG, Shihe YI, et al. · Chinese Journal of Aeronautics · 11
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Experimental investigation of supersonic turbulent flow over cylinders with various heights
2021 · Dundian Gang, Shihe Yi, et al. · Journal of Visualization · 11
Experimental investigation of the hypersonic boundary layer transition on a 7° straight cone
2018 · Liu Xiao-Lin, Yi Shi-He, et al. · Acta Physica Sinica · 11
Experimental study of crossflow instability in a Mach 6 delta wing flow
2021 · Hai-Bo Niu, Shi-He Yi, et al. · Acta Physica Sinica · 8
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Experimental Study on Unsteady Characteristics of Shock and Turbulent Boundary Layer Interactions
2020 · X. G. Lu, S. H. Yi, et al. · Fluid Dynamics · 7
Experimental Investigation of the Hypersonic Boundary Layer Transition on a 45° Swept Flat Plate
2020 · Xiaoge Lu, Shihe Yi, et al. · Fluid Dynamics · 7
Influence of laser-generated perturbations on hypersonic boundary-layer stability
2018 · Liu Xiao-Lin, Yi Shi-He, et al. · Acta Physica Sinica · 7
Aerodynamic optimization design of tandem-wing configurations based on multi-fidelity deep neural networks
2025 · Zilin Cai, Zhongjun Yu, et al. · Results in Engineering · 6
Flow Structure and Heat Flux Distribution of a Backswept Fin Induced Flow Field at M = 6
2020 · F. Zhang, S. H. Yi, et al. · Fluid Dynamics · 6
Experimental study of the high-frequency instability in the hypersonic boundary layer over a cone at 6° angle of attack
2022 · Haibo Niu, Shihe Yi, et al. · Acta Mechanica Sinica · 4
Experimental research on crossflow instability for a hypersonic 4∶1 elliptic cone
2021 · Wen-Peng Zheng, Shi-He Yi, et al. · Acta Physica Sinica · 4
Experimental study of the early evolution of traveling crossflow instability on a 75° swept flat plate at Mach 6
2024 · Haibo Niu, Shihe Yi, et al. · Physics of Fluids · 3
Experimental and Numerical Simulation Research on Boundary Layer Transition Front over a Swept Wing at M = 6
2021 · F. Zhang, S. H. Yi, et al. · Fluid Dynamics · 2
Visualization of supersonic flow over a rotating blunt cylinder at a high angle of attack
2021 · Dundian Gang, Shi-he Yi, et al. · Journal of Visualization · 1
Effect of Distributed Roughness Elements on Crossflow Transition in a Yawed Cone in a Mach 6 Wind Tunnel
2025 · Haibo Niu, Shihe Yi, et al. · Aerospace
Experimental and CFD investigation of the heat flux distribution and flow field structure on the leeward side of a 75∘ delta flat plate
2025 · Haibo Niu, Shihe Yi, et al. · Aerospace Science and Technology
Experimental investigation on the nonlinear development of the crossflow transition on a 75° swept flat plate at Mach 6
2025 · Haibo Niu, Shihe Yi, et al. · Physics of Fluids
Works count: 28
Citation count: 246
H-index: 11
I10-index: 11
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