Get started
Author

Dongsheng Zhang

Observed institution: Air Force Engineering University
ORCID: 0009-0005-4441-5739
Observed ORCID: 0009-0005-4441-5739
OpenAlex ID: A5125443174
Hypersonic shock–shock interaction over double wedge controlled by a supermultichannel high-energy pulsed arc discharge array
2024 · Dongsheng Zhang, Hesen Yang, et al. · Physics of Fluids · 9
Experimental study on hypersonic inlet flow separation controlled by plasma actuators
2026 · Dongsheng Zhang, Hesen Yang, et al. · Physics of Fluids · 2
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
Research on Shockwave/Boundary Layer Interactions Induced by Double Compression Corners Under Hypersonic Quiet and Noise Inflow Conditions
2025 · Dongsheng Zhang, Jinping Li, et al. · Aerospace · 1
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
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: 8
Citation count: 13
H-index: 2
I10-index:
Year
Topic
Type