E. R. Keener
About
In The Last Decade
E. R. Keener
42 papers receiving 621 citations
Peers
Comparison fields: 5 of 40
- Computational Mechanics 601
- Aerospace Engineering 424
- Applied Mathematics 154
- Environmental Engineering 84
- Ocean Engineering 57
Countries citing papers authored by E. R. Keener
This map shows the geographic impact of E. R. Keener'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 E. R. Keener with the expected number of citations based on a country's size and research output (numbers larger than one mean the country cites E. R. Keener more than expected).
Fields of papers citing papers by E. R. Keener
This network shows the impact of papers produced by E. R. Keener. 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 E. R. Keener. The network helps show where E. R. Keener may publish in the future.
Co-authorship network of co-authors of E. R. Keener
This figure shows the co-authorship network connecting the top 25 collaborators of E. R. Keener. A scholar is included among the top collaborators of E. R. Keener 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 E. R. Keener. E. R. Keener is excluded from the visualization to improve readability, since they are connected to all nodes in the network.
All Works
| # | Work | Indexed citations |
|---|---|---|
| 1 | 15 | |
| 2 | Pressure distributions and oil-flow patterns for a swept circulation-control wing | 2 |
| 3 | 1 | |
| 4 | Flow-separation patterns on symmetric forebodies | 47 |
| 5 | Boundary-layer measurements on a transonic low-aspect ratio wing | 3 |
| 6 | 4 | |
| 7 | Side forces on a tangent ogive forebody with a fineness ratio of 3.5 at high angles of attack and Mach numbers from 0.1 to 0.7 | 58 |
| 8 | 40 | |
| 9 | 94 | |
| 10 | 2 | |
| 11 | 2 | |
| 12 | 50 | |
| 13 | Direct measurements of turbulent skin friction on a nonadiabactic flat plate at Mach number 6.5 and comparisons with eight theories | 10 |
| 14 | Summary and Correlation of Skin-Friction and Heat-Transfer Data for a Hypersonic Turbulent Boundary Layer on Simple Shapes | 19 |
| 15 | 10 | |
| 16 | 1 | |
| 17 | Study of surface pitots for measuring turbulent skin friction at supersonic Mach numbers - Adiabatic wall | 27 |
| 18 | Flight evaluation of the x-15 ball-nose flow-direction sensor as an air-data system | 27 |
| 19 | Pressure measurements obtained in flight at transonic speeds for a conically cambered delta wing | 1 |
| 20 | Wind pressure distributions at low lift for the XF-92A delta-wing airplane at transonic speeds | 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.