Rowan Gollan
About
In The Last Decade
Rowan Gollan
80 papers receiving 883 citations
Peers
Comparison fields: 5 of 43
- Computational Mechanics 656
- Aerospace Engineering 511
- Applied Mathematics 487
- Fluid Flow and Transfer Processes 123
- Mechanical Engineering 87
Countries citing papers authored by Rowan Gollan
This map shows the geographic impact of Rowan Gollan'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 Rowan Gollan with the expected number of citations based on a country's size and research output (numbers larger than one mean the country cites Rowan Gollan more than expected).
Fields of papers citing papers by Rowan Gollan
This network shows the impact of papers produced by Rowan Gollan. 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 Rowan Gollan. The network helps show where Rowan Gollan may publish in the future.
Co-authorship network of co-authors of Rowan Gollan
This figure shows the co-authorship network connecting the top 25 collaborators of Rowan Gollan. A scholar is included among the top collaborators of Rowan Gollan 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 Rowan Gollan. Rowan Gollan is excluded from the visualization to improve readability, since they are connected to all nodes in the network.
All Works
| # | Work | Indexed citations |
|---|---|---|
| 1 | 2 | |
| 2 | 0 | |
| 3 | 2 | |
| 4 | 9 | |
| 5 | 27 | |
| 6 | 13 | |
| 7 | 2 | |
| 8 | 4 | |
| 9 | 2 | |
| 10 | Modeling Scramjet Supersonic Combustion Via Eddy Dissipation Model | 3 |
| 11 | 32 | |
| 12 | 37 | |
| 13 | 2 | |
| 14 | The Eilmer3 Code: user guide and example book | 11 |
| 15 | Adaption and use of a compressible flow code for turbomachinery design | 5 |
| 16 | 5 | |
| 17 | CFD Tools for Design and Simulation of Transient Flows in Hypersonic Facilities | 3 |
| 18 | 18 | |
| 19 | Impulse facility simulation of hypervelocity radiating flows | 5 |
| 20 | Numerical modelling of radiating superorbital flows: with detailed governing equations | 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.