Carl Trexler
About
In The Last Decade
Carl Trexler
30 papers receiving 515 citations
Peers
Comparison fields: 5 of 26
- Computational Mechanics 533
- Aerospace Engineering 473
- Applied Mathematics 201
- Fluid Flow and Transfer Processes 12
- Mechanical Engineering 8
Countries citing papers authored by Carl Trexler
This map shows the geographic impact of Carl Trexler'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 Carl Trexler with the expected number of citations based on a country's size and research output (numbers larger than one mean the country cites Carl Trexler more than expected).
Fields of papers citing papers by Carl Trexler
This network shows the impact of papers produced by Carl Trexler. 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 Carl Trexler. The network helps show where Carl Trexler may publish in the future.
Co-authorship network of co-authors of Carl Trexler
This figure shows the co-authorship network connecting the top 25 collaborators of Carl Trexler. A scholar is included among the top collaborators of Carl Trexler 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 Carl Trexler. Carl Trexler is excluded from the visualization to improve readability, since they are connected to all nodes in the network.
All Works
| # | Work | Indexed citations |
|---|---|---|
| 1 | 30 | |
| 2 | 3 | |
| 3 | 94 | |
| 4 | 15 | |
| 5 | 7 | |
| 6 | Propulsion Airframe Integration Test Techniques for Hypersonic Airbreathing Configurations at NASA Langley Research Center | 8 |
| 7 | Hypersonic Airbreathing Propulsion: An Aerodynamics, Aerothermodynamics, and Acoustics Competency White Paper | 5 |
| 8 | 3 | |
| 9 | 102 | |
| 10 | 1 | |
| 11 | 2 | |
| 12 | 3 | |
| 13 | 6 | |
| 14 | Instant-replay data system for combustion tests | 1 |
| 15 | Flameholding characteristics of a swept-strut H2 fuel-injector for scramjet applications | 8 |
| 16 | Characterization of a swept-strut hydrogen fuel-injector for scramjet applications | 3 |
| 17 | Wind-tunnel tests on a 3-dimensional fixed-geometry scramjet inlet at M = 2.30 to 4.60 | 1 |
| 18 | Design and performance at a local Mach number of 6 of an inlet for an integrated Scramjet concept. [wind tunnel models - aircraft design | 7 |
| 19 | Design and performance at a local Mach number of 6 of an inlet for an integrated Scramjet concept | 33 |
| 20 | Preliminary investigation of momentum diffusion between two supersonic airstreams in the presence of shock waves | 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.