World's Best Scientists 2026 revealed!

D-Index & Metrics

Mechanical and Aerospace Engineering

D-Index
57
Citations
10338
World Ranking
818
National Ranking
105

Overview

Zhenguo Wang is affiliated with the National University of Defense Technology in China. Their research primarily focuses on engineering, with a particular emphasis on computational mechanics and aerospace engineering. The scope of their work also includes electrical and electronic engineering, fluid flow and transfer processes, and radiology, nuclear medicine, and imaging.

The main research topics Zhenguo Wang has explored include computational fluid dynamics and aerodynamics, combustion and flame dynamics, plasma and flow control in aerodynamics, fluid dynamics and turbulent flows, rocket and propulsion systems research, combustion and detonation processes, and plasma applications and diagnostics.

Wang has published extensively in several scientific venues. Frequent publication platforms include Aerospace Science and Technology, AIAA Journal, Physics of Fluids, Combustion and Flame, and Chinese Journal of Aeronautics.

Coauthorship collaborations have been significant in Wang's work, with frequent coauthors being Mingbo Sun, Hongbo Wang, Jiajian Zhu, Zun Cai, and Rong Feng.

Selected recent papers authored or coauthored by Zhenguo Wang include:

  • Suppression of combustion mode transitions in a hydrogen-fueled scramjet combustor by a multi-channel gliding arc plasma (2021, Combustion and Flame)
  • Ignition and combustion enhancement in a cavity-based supersonic combustor by a multi-channel gliding arc plasma (2020, Experimental Thermal and Fluid Science)
  • Flame stabilization enhancement in a strut-based supersonic combustor by shock wave generators (2020, Aerospace Science and Technology)
  • Ignition modes of a cavity-based scramjet combustor by a gliding arc plasma (2020, Energy)
  • Combustion Characteristics in Scramjet Combustor Operating at Different Inflow Stagnation Pressures (2022, AIAA Journal)

Best Publications

  • Influences of the turbulence model and the slot width on the transverse slot injection flow field in supersonic flows

    Wei Huang;Wei-dong Liu;Shi-bin Li;Zhi-xun Xia

  • Combustion modes of hydrogen jet combustion in a cavity-based supersonic combustor

    Hongbo Wang;Zhenguo Wang;Mingbo Sun;Haiyan Wu

  • Flame Characteristics in Supersonic Combustor with Hydrogen Injection Upstream of Cavity Flameholder

    Ming-Bo Sun;Zhen-Guo Wang;Jian-Han Liang;Hui Geng

  • Performance evaluation and parametric analysis on cantilevered ramp injector in supersonic flows

    Wei Huang;Shi-bin Li;Li Yan;Zhen-guo Wang

  • Mixing-related low frequency oscillation of combustion in an ethylene-fueled supersonic combustor

    Zhen-guo Wang;Ming-bo Sun;Hong-bo Wang;Jiang-fei Yu

  • Large eddy simulation of a hydrogen-fueled scramjet combustor with dual cavity

    Hongbo Wang;Zhenguo Wang;Mingbo Sun;Ning Qin

  • Combustion characteristics in a supersonic combustor with hydrogen injection upstream of cavity flameholder

    Hongbo Wang;Zhenguo Wang;Mingbo Sun;Ning Qin

  • Experimental investigation on drag and heat flux reduction in supersonic/hypersonic flows: A survey

    Zhen-guo Wang;Xi-wan Sun;Wei Huang;Shi-bin Li

  • Numerical investigation on the shock wave transition in a three-dimensional scramjet isolator

    Wei Huang;Wei Huang;Zhen-guo Wang;Mohamed Pourkashanian;Lin Ma

  • Overview of the key technologies of combined cycle engine precooling systems and the advanced applications of micro-channel heat transfer

    Zhen-guo Wang;Yuan Wang;Jian-qiang Zhang;Bei-chen Zhang

  • Review of cavity-stabilized combustion for scramjet applications:

    Zhenguo Wang;Hongbo Wang;Mingbo Sun

  • Large-Eddy/Reynolds-averaged Navier–Stokes simulation of combustion oscillations in a cavity-based supersonic combustor

    Hongbo Wang;Zhenguo Wang;Mingbo Sun;Ning Qin

  • Parametric effects on the combustion flow field of a typical strut-based scramjet combustor

    Wei Huang;Wei Huang;ZhenGuo Wang;ShiBin Luo;Jun Liu

  • Experimental study of oscillations in a scramjet combustor with cavity flameholders

    Hongbo Wang;Zhenguo Wang;Mingbo Sun

  • Suppression of combustion mode transitions in a hydrogen-fueled scramjet combustor by a multi-channel gliding arc plasma

    Rong Feng;Jiajian Zhu;Zhenguo Wang;Fan Zhang

  • Effect of geometric parameters on the drag of the cavity flameholder based on the variance analysis method

    Wei Huang;Wei Huang;Mohamed Pourkashanian;Lin Ma;Derek B. Ingham

  • Effect of cavity flame holder configuration on combustion flow field performance of integrated hypersonic vehicle

    Wei Huang;ShiBin Luo;Jun Liu;ZhenGuo Wang

  • Winglet design for vertical axis wind turbines based on a design of experiment and CFD approach

    Tian-tian Zhang;Tian-tian Zhang;Mohamed Elsakka;Mohamed Elsakka;Wei Huang;Zhen-guo Wang

  • Experiments on flame stabilization in a scramjet combustor with a rear-wall-expansion cavity

    Zun Cai;Xiaobin Zhu;Mingbo Sun;Zhenguo Wang

  • Ignition and combustion enhancement in a cavity-based supersonic combustor by a multi-channel gliding arc plasma

    Rong Feng;Yuhui Huang;Jiajian Zhu;Zhenguo Wang

  • Design exploration for a single expansion ramp nozzle (SERN) using data mining

    Wei Huang;Zhen-guo Wang;Derek B. Ingham;Lin Ma

  • Numerical prediction on the interaction between the incident shock wave and the transverse slot injection in supersonic flows

    Wei Huang;Zhen-guo Wang;Ji-ping Wu;Shi-bin Li

  • Influences of H2O mass fraction and chemical kinetics mechanism on the turbulent diffusion combustion of H2–O2 in supersonic flows

    Wei Huang;Zhen-guo Wang;Shi-bin Li;Wei-dong Liu

Frequent Co-Authors

Wei Huang
Wei Huang National University of Defense Technology
Derek B. Ingham
Derek B. Ingham University of Sheffield
Xue-Song Bai
Xue-Song Bai Lund University
Ning Qin
Ning Qin University of Sheffield
Lin Ma
Lin Ma University of Sheffield
Mohamed Pourkashanian
Mohamed Pourkashanian University of Sheffield
Wei Liu
Wei Liu Sun Yat-sen University
Khellil Sefiane
Khellil Sefiane University of Edinburgh
Bengt Sundén
Bengt Sundén Lund University
John H.S. Lee
John H.S. Lee McGill University

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