M. L. Mason
About
In The Last Decade
M. L. Mason
25 papers receiving 325 citations
Peers
Comparison fields: 5 of 34
- Computational Mechanics 306
- Aerospace Engineering 281
- Applied Mathematics 84
- Astronomy and Astrophysics 19
- Control and Systems Engineering 12
Countries citing papers authored by M. L. Mason
This map shows the geographic impact of M. L. Mason'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 M. L. Mason with the expected number of citations based on a country's size and research output (numbers larger than one mean the country cites M. L. Mason more than expected).
Fields of papers citing papers by M. L. Mason
This network shows the impact of papers produced by M. L. Mason. 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 M. L. Mason. The network helps show where M. L. Mason may publish in the future.
Co-authorship network of co-authors of M. L. Mason
This figure shows the co-authorship network connecting the top 25 collaborators of M. L. Mason. A scholar is included among the top collaborators of M. L. Mason 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 M. L. Mason. M. L. Mason is excluded from the visualization to improve readability, since they are connected to all nodes in the network.
All Works
| # | Work | Indexed citations |
|---|---|---|
| 1 | 65 | |
| 2 | 55 | |
| 3 | 5 | |
| 4 | Multiaxis thrust vectoring using axisymmetric nozzles and postexit vanes on an F/A-18 configuration vehicle | 18 |
| 5 | The Measurement of Large Ducted Gas Flows | 2 |
| 6 | 2 | |
| 7 | An experimental investigation of thrust vectoring two-dimensional convergent-divergent nozzles installed in a twin-engine fighter model at high angles of attack | 8 |
| 8 | Transonic Navier-Stokes solutions of three-dimensional afterbody flows | 10 |
| 9 | 2 | |
| 10 | Static performance of nonaxisymmetric nozzles with yaw thrust-vectoring vanes | 8 |
| 11 | 8 | |
| 12 | 9 | |
| 13 | Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability | 1 |
| 14 | 3 | |
| 15 | Experimental investigation of two nonaxisymmetric wedge nozzles at free stream Mach numbers up to 1.20 | 2 |
| 16 | Pitot pressure measurements in flow fields behind circular-arc nozzles with exhaust jets at subsonic free-stream Mach numbers | 4 |
| 17 | Experimental and analytical investigation of a nonaxisymmetric wedge nozzle at static conditions | 2 |
| 18 | 17 | |
| 19 | Accuracy of estimating the masses of Phobos and Deimos from multiple Viking Orbiter encounters. | 1 |
| 20 | Accuracy of estimating the masses of Phobos and Deimos from multiple Viking orbiter encounters | 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.