Zhenguo Wang
About
In The Last Decade
Zhenguo Wang
106 papers receiving 2.9k citations
Peers
Comparison fields: 5 of 70
- Computational Mechanics 2.5k
- Aerospace Engineering 1.8k
- Applied Mathematics 303
- Fluid Flow and Transfer Processes 303
- Ocean Engineering 197
Countries citing papers authored by Zhenguo Wang
This map shows the geographic impact of Zhenguo Wang'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 Zhenguo Wang with the expected number of citations based on a country's size and research output (numbers larger than one mean the country cites Zhenguo Wang more than expected).
Fields of papers citing papers by Zhenguo Wang
This network shows the impact of papers produced by Zhenguo Wang. 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 Zhenguo Wang. The network helps show where Zhenguo Wang may publish in the future.
Co-authorship network of co-authors of Zhenguo Wang
This figure shows the co-authorship network connecting the top 25 collaborators of Zhenguo Wang. A scholar is included among the top collaborators of Zhenguo Wang 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 Zhenguo Wang. Zhenguo Wang is excluded from the visualization to improve readability, since they are connected to all nodes in the network.
All Works
| # | Work | Indexed citations |
|---|---|---|
| 1 | 9 | |
| 2 | 0 | |
| 3 | 14 | |
| 4 | 38 | |
| 5 | 65 | |
| 6 | 125 | |
| 7 | Experiment on liquid sheet breakup process of pressure swirl injector | 4 |
| 8 | An Uncoupled Method with Dual Time-step for Chemical Nonequilibrium Flows | 4 |
| 9 | EVALUATION OF PARTIALLY PREMIXED FLAMELET APPROACH IN SUPERSONIC COMBUSTION | 2 |
| 10 | Comparison of characteristics of ramjet with cavity-based flameholder and V-gutter flameholder | 5 |
| 11 | Analysis of Internal Drag of Scramjet Engine with Multi-cavities in Tandem | 2 |
| 12 | Experimental Investigation of Effects on Ignition in an Axisymmetric Ramjet Combustor Based on Cavity | 2 |
| 13 | An integrated optimization of hypersonic forebody/inlet based on surrogate models | 3 |
| 14 | Experimental on control of liquid hydrocarbon fueled scramjet combustor | 1 |
| 15 | Numerical Simulation of the Effect of Viscosity on the Performance of Hypersonic Vehicle | 3 |
| 16 | The Analysis on the Multidisciplinary Design Optimization Process for Satellite System | 2 |
| 17 | The Multi-level and Multiobjective Optimization Design Method for Two Dimensional Scramjet Inlet | 3 |
| 18 | Experimental investigation of ignition technology in liquid hydrocarbon fueled scramjet combustor | 4 |
| 19 | Experimental Study of Supersonic Combustion of Kerosene | 1 |
| 20 | Response of Propellant Droplet Subcritical Evaporation to Environmental Pressure Oscillation | 1 |
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.