T. A. Weisshaar
About
In The Last Decade
T. A. Weisshaar
34 papers receiving 444 citations
Peers
Comparison fields: 5 of 45
- Aerospace Engineering 361
- Mechanics of Materials 238
- Civil and Structural Engineering 186
- Computational Mechanics 100
- Control and Systems Engineering 92
Countries citing papers authored by T. A. Weisshaar
This map shows the geographic impact of T. A. Weisshaar'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 T. A. Weisshaar with the expected number of citations based on a country's size and research output (numbers larger than one mean the country cites T. A. Weisshaar more than expected).
Fields of papers citing papers by T. A. Weisshaar
This network shows the impact of papers produced by T. A. Weisshaar. 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 T. A. Weisshaar. The network helps show where T. A. Weisshaar may publish in the future.
Co-authorship network of co-authors of T. A. Weisshaar
This figure shows the co-authorship network connecting the top 25 collaborators of T. A. Weisshaar. A scholar is included among the top collaborators of T. A. Weisshaar 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 T. A. Weisshaar. T. A. Weisshaar is excluded from the visualization to improve readability, since they are connected to all nodes in the network.
All Works
| # | Work | Indexed citations |
|---|---|---|
| 1 | 54 | |
| 2 | 38 | |
| 3 | Adaptive Wing Flexural Axis Control | 7 |
| 4 | Static aeroelastic control of an adaptive lifting surface | 3 |
| 5 | 29 | |
| 6 | Adaptive Static and Dynamic Aeroelastic Design | 6 |
| 7 | Integrated structure/control design - Present methodology and future opportunities | 10 |
| 8 | STRUCTURAL TAILORING FOR AIRCRAFT PERFORMANCE | 2 |
| 9 | 3 | |
| 10 | Interactive aircraft flight control and aeroelastic stabilization | 0 |
| 11 | 13 | |
| 12 | On the track of practical forward-swept wings | 19 |
| 13 | Aeroelastic Tailoring with Composites Applied to Forward Swept Wings | 10 |
| 14 | 3 | |
| 15 | 24 | |
| 16 | 3 | |
| 17 | 1 | |
| 18 | 15 | |
| 19 | 15 | |
| 20 | 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.