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Author

Hua Liang

Observed name: Hua LIANG
ORCID: 0000-0002-0281-3094
Observed ORCIDs: 0000-0002-0281-3094, 0000-0003-2547-2701
OpenAlex ID: A5125457700
Experimental study on hypersonic inlet flow separation controlled by plasma actuators
2026 · Dongsheng Zhang, Hesen Yang, et al. · Physics of Fluids · 2
Optimization of rotor aerodynamic performance via machine learning-based plasma flow control
2026 · Fuyao ZHANG, Hesen YANG, et al. · Chinese Journal of Aeronautics · 1
Experimental investigation on the inlet shock wave/boundary layer interaction controlled by pulsed arc plasma discharge
2026 · Xinyu Kong, Zhi Su, et al. · Aerospace Science and Technology · 1
Experimental study on incident shock wave/boundary layer interaction controlled by pulsed arc discharge
2026 · Mingrui Lu, Zhi Su, et al. · Aerospace Science and Technology · 1
Shock wave/boundary layer interaction control at different geometrical parameters using pulsed spark discharge array
2026 · Mingrui LU, Mengxiao TANG, et al. · Chinese Journal of Aeronautics
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Direct numerical simulation of plasma-based control for separation induced by hypersonic shock wave/boundary layer interaction
2026 · Botian Zhang, Haohua Zong, et al. · Aerospace Science and Technology
Control of shock wave/boundary layer interaction over a supersonic compression corner using alternating continuous plasma actuation
2026 · Dongsheng Zhang, Haohua Zong, et al. · Physics of Fluids
Mechanisms of plasma actuation on hypersonic boundary-layer instability and mode evolution
2026 · Zhehao Li, Caihong Su, et al. · Acta Mechanica Sinica
Flight demonstration of closed-loop skin-friction drag reduction with reinforcement learning
2026 · Ziqi Fang, Haohua Zong, et al. · Aerospace Science and Technology
Experimental research on supersonic shock wave/boundary layer interaction controlled by alternating continuous plasma actuation
2026 · Dongsheng Zhang, Haohua Zong, et al. · Aerospace Science and Technology
Experimental study on nanosecond pulsed discharge mode transition in supersonic flow with needle-to-plate electrodes
2026 · Fuyao Zhang, Shengwu Zhang, et al. · Journal of Applied Physics
Plasma-based experimental investigation of compression corner shock wave/boundary layer interaction control under hypersonic quiet and noise inflow conditions
2026 · Dongsheng Zhang, Hesen Yang, et al. · Physics of Plasmas
Works count: 12
Citation count: 5
H-index: 1
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