Guoyan Zhao

967 total citations
50 papers, 708 citations indexed

About

Guoyan Zhao is a scholar working on Computational Mechanics, Aerospace Engineering and Applied Mathematics. According to data from OpenAlex, Guoyan Zhao has authored 50 papers receiving a total of 708 indexed citations (citations by other indexed papers that have themselves been cited), including 49 papers in Computational Mechanics, 19 papers in Aerospace Engineering and 8 papers in Applied Mathematics. Recurrent topics in Guoyan Zhao's work include Computational Fluid Dynamics and Aerodynamics (48 papers), Combustion and flame dynamics (36 papers) and Fluid Dynamics and Turbulent Flows (20 papers). Guoyan Zhao is often cited by papers focused on Computational Fluid Dynamics and Aerodynamics (48 papers), Combustion and flame dynamics (36 papers) and Fluid Dynamics and Turbulent Flows (20 papers). Guoyan Zhao collaborates with scholars based in China and Italy. Guoyan Zhao's co-authors include Mingbo Sun, Hongbo Wang, Tao Tang, Sergio Pirozzoli, Jiangfei Yu, Dapeng Xiong, Yuhui Huang, Zhenguo Wang, Jiajian Zhu and Fan Li and has published in prestigious journals such as Journal of Computational Physics, International Journal of Hydrogen Energy and Energy.

In The Last Decade

Guoyan Zhao

45 papers receiving 682 citations

Peers — A (Enhanced Table)

Peers by citation overlap · career bar shows stage (early→late) cites · hero ref

Name h Career Trend Papers Cites
Guoyan Zhao China 17 649 383 84 75 27 50 708
Yongchao Sun China 11 374 0.6× 233 0.6× 27 0.3× 79 1.1× 24 0.9× 33 436
Jiangfei Yu China 15 691 1.1× 427 1.1× 62 0.7× 188 2.5× 23 0.9× 31 736
Heeseok Koo United States 13 509 0.8× 236 0.6× 148 1.8× 157 2.1× 29 1.1× 30 581
Toshinori Kouchi Japan 16 679 1.0× 484 1.3× 115 1.4× 32 0.4× 19 0.7× 93 747
Zhao-bo Du China 19 1.1k 1.7× 847 2.2× 168 2.0× 57 0.8× 26 1.0× 31 1.2k
Luca Maddalena United States 15 541 0.8× 368 1.0× 143 1.7× 18 0.2× 32 1.2× 69 630
M. A. Goldfeld Russia 11 362 0.6× 314 0.8× 85 1.0× 27 0.4× 16 0.6× 75 416
Kemal Yuceil United States 12 725 1.1× 575 1.5× 239 2.8× 30 0.4× 12 0.4× 18 816
Tetsuo Hiraiwa Japan 15 620 1.0× 551 1.4× 262 3.1× 96 1.3× 44 1.6× 58 716
L. Gasparini Italy 4 376 0.6× 248 0.6× 159 1.9× 18 0.2× 42 1.6× 7 464

Countries citing papers authored by Guoyan Zhao

Since Specialization
Citations

This map shows the geographic impact of Guoyan Zhao's research. It shows the number of citations coming from papers published by authors working in each country. You can also color the map by specialization and compare the number of citations received by Guoyan Zhao with the expected number of citations based on a country's size and research output (numbers larger than one mean the country cites Guoyan Zhao more than expected).

Fields of papers citing papers by Guoyan Zhao

Since Specialization
Physical SciencesHealth SciencesLife SciencesSocial Sciences

This network shows the impact of papers produced by Guoyan Zhao. Nodes represent research fields, and links connect fields that are likely to share authors. Colored nodes show fields that tend to cite the papers produced by Guoyan Zhao. The network helps show where Guoyan Zhao may publish in the future.

Co-authorship network of co-authors of Guoyan Zhao

This figure shows the co-authorship network connecting the top 25 collaborators of Guoyan Zhao. A scholar is included among the top collaborators of Guoyan Zhao based on the total number of citations received by their joint publications. Widths of edges represent the number of papers authors have co-authored together. Node borders signify the number of papers an author published with Guoyan Zhao. Guoyan Zhao is excluded from the visualization to improve readability, since they are connected to all nodes in the network.

All Works

20 of 20 papers shown
1.
Zhao, Guoyan, et al.. (2025). Scale effect numerical investigation of supersonic cavity-based combustors under different combustion modes. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering. 239(15). 2102–2115. 1 indexed citations
2.
Zhao, Guoyan, et al.. (2025). Weak heat release and complex combustion transitions in high-Mach scramjet combustor. Applied Thermal Engineering. 280. 128318–128318.
3.
Zhao, Guoyan, et al.. (2025). The shock-assisted self-ignition behavior and combustion transition mechanisms in a Mach 8 scramjet combustor. Combustion and Flame. 285. 114721–114721.
4.
Zhao, Guoyan, et al.. (2025). Transition dynamics of ethylene combustion in a Mach 8 scramjet combustor: From autoignition to flame stabilization. International Communications in Heat and Mass Transfer. 166. 109201–109201. 2 indexed citations
5.
Zhao, Guoyan, et al.. (2025). Application of Throat Compensation Based on Scale Effects of the Scramjet Combustor. AIAA Journal. 63(10). 4357–4373.
6.
Zhao, Guoyan, et al.. (2024). On scale effect of supersonic combustion in axisymmetric combustor. Aerospace Science and Technology. 155. 109566–109566. 5 indexed citations
7.
Li, Fan, et al.. (2024). On the scale effects of flame stabilization under different combustion modes in an ethylene-fueled scramjet combustor. Combustion and Flame. 270. 113725–113725. 10 indexed citations
8.
Li, Fan, et al.. (2024). Effect of Gas Addition on Liquid Kerosene Combustion in a Scramjet Combustor. AIAA Journal. 62(9). 3284–3293. 3 indexed citations
9.
Zhao, Guoyan, et al.. (2024). On compression level of hypersonic airflow in high-mach scramjet. Energy. 295. 130993–130993. 8 indexed citations
10.
Zhao, Guoyan, et al.. (2024). Role of cavity in a Mach 8 axisymmetric scramjet combustor: Flame stabilization vs combustion enhancement. Physics of Fluids. 36(1). 20 indexed citations
11.
Li, Fan, et al.. (2024). Effect of injection distance on supersonic combustion under different combustion modes. Physics of Fluids. 36(11). 2 indexed citations
12.
Tang, Tao, Jiangfei Yu, Yuhui Huang, et al.. (2023). Numerical study of transverse jet mixing and combustion in a high-enthalpy supersonic crossflow with trace gases. Physics of Fluids. 35(3). 23 indexed citations
13.
Tang, Tao, Jiangfei Yu, Zhenguo Wang, et al.. (2023). An improved flamelet/progress variable modeling in a hydrogen-fueled scramjet. International Journal of Hydrogen Energy. 49. 77–91. 9 indexed citations
14.
Tang, Tao, Zhenguo Wang, Hesong Li, et al.. (2022). A method for optimizing reaction progress variable and its application. Aerospace Science and Technology. 130. 107888–107888. 6 indexed citations
15.
Zhao, Guoyan, et al.. (2021). Effects of injection on flame flashback in supersonic crossflow. Aerospace Science and Technology. 120. 107226–107226. 24 indexed citations
16.
Li, Liang, Hongbo Wang, Dapeng Xiong, et al.. (2020). An Adaptive High-Resolution and Low-Dissipation Hybrid Energy Consistent/WENOCU Scheme. IOP Conference Series Materials Science and Engineering. 790(1). 12078–12078. 1 indexed citations
17.
Li, Liang, Hongbo Wang, Guoyan Zhao, et al.. (2020). An Efficient Low-Dissipation Hybrid Central/WENO Scheme for Compressible Flows. International journal of computational fluid dynamics. 34(10). 705–730. 14 indexed citations
18.
Zhao, Guoyan, Mingbo Sun, Yong Mei, et al.. (2019). An Efficient Adaptive Central-Upwind WENO-CU6 Numerical Scheme with a New Sensor. Journal of Scientific Computing. 81(2). 649–670. 19 indexed citations
19.
Zhao, Guoyan, et al.. (2018). A general framework for the evaluation of shock-capturing schemes. Journal of Computational Physics. 376. 924–936. 32 indexed citations
20.
Zhao, Guoyan, et al.. (2018). Investigations of injection parameters on combustion oscillation in a supersonic crossflow. Acta Astronautica. 152. 426–436. 17 indexed citations

Rankless uses publication and citation data sourced from OpenAlex, an open and comprehensive bibliographic database. While OpenAlex provides broad and valuable coverage of the global research landscape, it—like all bibliographic datasets—has inherent limitations. These include incomplete records, variations in author disambiguation, differences in journal indexing, and delays in data updates. As a result, some metrics and network relationships displayed in Rankless may not fully capture the entirety of a scholar's output or impact.

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