Wangyuhui头像

Wangyuhui

Associate professor

Research direction: Detonation, shock wave

100029

Education:

  • Department: College of Mechanical and Electrical Engineering
  • ORCID: 0000-0002-9805-2583
  • DBLP:

10 Access

  • Email: aowuki@163.com
  • Office : Room 402, Mechanical Building

Introduction

Yuhui Wang is a professor at the School of Mechanical and Electrical Engineering, Beijing University of Chemical Technology. He received his Ph. D. in fluid mechanics from Peking University. His research interests are combustion flow, vibration, noise and heat transfer in engines, as well as detonation and shock waves.

Education

Work Experience

Social Position

Social Activities

Research

detonation and shock waves

Teaching

Theoretical mechanics and elastic mechanics

Postgraduates

Funding

Research on Mid-frequency instability of Rotating Detonation, National Natural Science Foundation of China, 11602207, 201701-201912.


Vertical Project

Horizontal Project

Publications

1.        Sun, F., Song, Y., Wang, Y. *, Zhang, Y.*. (2024). Improved mixing-width model for the linear stage of reshocked Richtmyer–Meshkov turbulence. Phys. Fluids, 36: 085201.

2.        Jiang, C., Wang, Y.*. (2024). Pressure-angle polars obtaining flow field of rotating detonation. Combust. Sci. Technol., 1962020-2037.

3.        Zhu, W., Wang, Y.*, Wang, J. (2022). Flow field of a rotating detonation engine fueled by carbon. Phys. Fluids, 34: 073311.

4.        Zhu, W., Wang, Y.*. (2022). Effect of hydrogen flow rate and particle diameter on coal-hydrogen-air rotating detonation engines. Int. J. Hydrogen Energy, 47: 1328-1342.

5.        Wang, Y. *, Le, J. (2022). Experimental study of sharp noise caused by rotating detonation waves. Noise Control Engr. J., 70: 527-539.

6.        Wang, Y. *, Le, J. (2021). Combustion characteristics in rotating detonation engines. Int. J. Aerosp. Eng., 2021, 8839967.

7.        Wang, Y. *, Le, J. (2021). A rotating detonation engine using methane-ethylene mixture and air. Acta Astronaut., 188: 25-35.

8.        Wang, Y. *, Le, J. (2019). A hollow combustor that intensifies rotating detonation. Aerosp. Sci. Technol., 85:113-124.

9.        Wang, Y. *, Le, J. (2019). Rotating detonation engines with two fuel orifice schemes. Acta Astronaut., 161: 262-275.

10.     Wang, Y. *, Le, J., Wang, C., Zheng, Y., Huang, S. (2019). The effect of the throat width of plug nozzles on the combustion mode in rotating detonation engines. Shock Waves, 29: 471-485.

11.     Wang, Y. *, Le, J., Wang, C., Zheng, Y. (2018). A non-premixed rotating detonation engine using ethylene and air. Appl. Therm. Eng., 137: 749-757.


Awards

1. World's Top 2% Scientists,2023-2024.

2.The 17th Beijing Youth Outstanding scientific and Technological paper, 2024.

Patent

Honor Reward

Admissions Information