R. D. Moore
About
In The Last Decade
R. D. Moore
45 papers receiving 749 citations
Peers
Comparison fields: 5 of 42
- Aerospace Engineering 646
- Computational Mechanics 412
- Mechanical Engineering 366
- Mechanics of Materials 88
- Electrical and Electronic Engineering 53
Countries citing papers authored by R. D. Moore
This map shows the geographic impact of R. D. Moore'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. D. Moore with the expected number of citations based on a country's size and research output (numbers larger than one mean the country cites R. D. Moore more than expected).
Fields of papers citing papers by R. D. Moore
This network shows the impact of papers produced by R. D. Moore. 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. D. Moore. The network helps show where R. D. Moore may publish in the future.
Co-authorship network of co-authors of R. D. Moore
This figure shows the co-authorship network connecting the top 25 collaborators of R. D. Moore. A scholar is included among the top collaborators of R. D. Moore 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. D. Moore. R. D. Moore is excluded from the visualization to improve readability, since they are connected to all nodes in the network.
All Works
| # | Work | Indexed citations |
|---|---|---|
| 1 | Aerodynamic Performance of Axial-Flow Fan Stage Operated at Nine Inlet Guide Vane Angles | 0 |
| 2 | The Alternative Low Noise Fan | 2 |
| 3 | 1 | |
| 4 | Experimental Evaluation of Turning Vane Designs for High-speed and Coupled Fan-drive Corners of 0.1-scale Model of NASA Lewis Research Center's Proposed Altitude Wind Tunnel | 1 |
| 5 | 18 | |
| 6 | 13 | |
| 7 | Comparison of analytical and experimental performance of a wind-tunnel diffuser section | 1 |
| 8 | 10 | |
| 9 | Aerodynamic performance of 1.38-pressure-ratio, variable-pitch fan stage | 4 |
| 10 | Experimental study of low aspect ratio compressor blading | 0 |
| 11 | Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.19 and 1.26, respectively, and with design pressure ratio of 1.82 | 69 |
| 12 | Aerodynamic performance of a 1.35-pressure-ratio axial-flow fan stage | 4 |
| 13 | Aerodynamic performance of a 1.20-pressure ratio fan stage designed for low noise | 1 |
| 14 | Performance of a low-pressure fan stage with reverse flow | 1 |
| 15 | Hydrogen cavitation performance of 80.6 deg helical inducer mounted in line with stationary centerbody | 2 |
| 16 | Hydrogen cavitation performance of 80.6 deg helical inducer with blunt leading edges | 0 |
| 17 | 31 | |
| 18 | Venturi scaling studies on thermodynamic effects of developed cavitation of Freon-114 | 2 |
| 19 | Effects of wall pressure distribution and liquid temperature on incipient cavitation of Freon-114 and water in venturi flow | 2 |
| 20 | 0 |
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.