Author

Yun Wu

Institution: Air Force Engineering University

Observed institution: Air Force Engineering University

ORCID: 0000-0002-3014-6620

Observed ORCID: 0000-0002-3014-6620

OpenAlex ID: A5123554344

Experimental study on heat release characteristics and performance parameters of two-phase rotating detonation combustor under different equivalence ratios and outlet area ratios

2026 · Liming Liu, Jiaojiao Wang, et al. · Applied Thermal Engineering · 4

Ignition and combustion enhancement of kerosene spray flames by AC powered multichannel gliding arc discharges

2026 · Shengfang Huang, Yun Wu, et al. · Aerospace Science and Technology · 1

Comparison of dual-mode gliding-arc plasma actuation for lean ignition and lean blowout in a cavity-strut afterburner combustor

2026 · Xing Zheng, Huifeng Miao, et al. · Aerospace Science and Technology

Effects of inflow total temperature on the operating characteristics of a liquid kerosene fueled rotating detonation combustor

2026 · Yibing Chang, Shanguang Guo, et al. · Acta Astronautica

Generating Coupled Total Pressure and Swirl Distortions Using S-Duct Plate

2026 · Haideng Zhang, Yun Wu, et al. · Journal of Engineering for Gas Turbines and Power

Active control of the flow field characteristics behind a bluff body by multichannel nanosecond-pulsed discharges

2026 · Shengfang Huang, Yun Wu, et al. · Physics of Fluids

Aerodynamic Performance of Plasma-Actuated Supersonic Compressor Airfoil at Low Reynolds Number

2026 · Tangyi Zhang, Haideng Zhang, et al. · SSRN Electronic Journal

Works count: 7

Citation count: 5

H-index: 1

I10-index: