R. M. Hicks
About
In The Last Decade
R. M. Hicks
49 papers receiving 1.5k citations
Hit Papers
Peers
Comparison fields: 5 of 49
- Computational Mechanics 1.1k
- Aerospace Engineering 712
- Computational Theory and Mathematics 304
- Statistics, Probability and Uncertainty 270
- Applied Mathematics 251
Countries citing papers authored by R. M. Hicks
This map shows the geographic impact of R. M. Hicks'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 R. M. Hicks with the expected number of citations based on a country's size and research output (numbers larger than one mean the country cites R. M. Hicks more than expected).
Fields of papers citing papers by R. M. Hicks
This network shows the impact of papers produced by R. M. Hicks. 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 R. M. Hicks. The network helps show where R. M. Hicks may publish in the future.
Co-authorship network of co-authors of R. M. Hicks
This figure shows the co-authorship network connecting the top 25 collaborators of R. M. Hicks. A scholar is included among the top collaborators of R. M. Hicks 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 R. M. Hicks. R. M. Hicks is excluded from the visualization to improve readability, since they are connected to all nodes in the network.
All Works
| # | Work | Indexed citations |
|---|---|---|
| 1 | 19 | |
| 2 | 50 | |
| 3 | 29 | |
| 4 | 1 | |
| 5 | 8 | |
| 6 | 2 | |
| 7 | Computerized three-dimensional aerodynamic design of a lifting rotor blade | 4 |
| 8 | 10 | |
| 9 | Supercritical wing design using numerical optimization and comparisons with experiment | 11 |
| 10 | 2 | |
| 11 | 4 | |
| 12 | Wing analysis using a transonic potential flow computational method | 12 |
| 13 | 57 | |
| 14 | 37 | |
| 15 | Pressure signatures for the Apollo command module and the Saturn 5 launch vehicle with a discussion of strong shock extrapolation procedures | 2 |
| 16 | A Wind Tunnel Flight Correlation of Apollo 15 Sonic Boom | 2 |
| 17 | On the extrapolation of measured near field pressure signatures of unconventional configurations | 1 |
| 18 | Further studies of the extrapolation of near field overpressure data | 12 |
| 19 | Transition fixing for hypersonic flow | 15 |
| 20 | 2 |
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.