Joseph Vadyak
About
In The Last Decade
Joseph Vadyak
30 papers receiving 279 citations
Peers
Comparison fields: 5 of 30
- Computational Mechanics 277
- Aerospace Engineering 224
- Applied Mathematics 40
- Environmental Engineering 17
- Statistical and Nonlinear Physics 16
Countries citing papers authored by Joseph Vadyak
This map shows the geographic impact of Joseph Vadyak'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 Joseph Vadyak with the expected number of citations based on a country's size and research output (numbers larger than one mean the country cites Joseph Vadyak more than expected).
Fields of papers citing papers by Joseph Vadyak
This network shows the impact of papers produced by Joseph Vadyak. 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 Joseph Vadyak. The network helps show where Joseph Vadyak may publish in the future.
Co-authorship network of co-authors of Joseph Vadyak
This figure shows the co-authorship network connecting the top 25 collaborators of Joseph Vadyak. A scholar is included among the top collaborators of Joseph Vadyak 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 Joseph Vadyak. Joseph Vadyak is excluded from the visualization to improve readability, since they are connected to all nodes in the network.
All Works
| # | Work | Indexed citations |
|---|---|---|
| 1 | Navier-Stokes Computations of the Full V-22 Configuration Using Massively Parallel Computers | 3 |
| 2 | 10 | |
| 3 | 72 | |
| 4 | 20 | |
| 5 | Computation of aircraft component flow fields at transonic Mach numbers using a three-dimensional Navier-Stokes algorithm | 3 |
| 6 | 3 | |
| 7 | 40 | |
| 8 | 2 | |
| 9 | 19 | |
| 10 | 3 | |
| 11 | 4 | |
| 12 | 9 | |
| 13 | 25 | |
| 14 | 2 | |
| 15 | 3 | |
| 16 | 26 | |
| 17 | A computer program for the calculation of the flow field including boundary layer effects for mixed-compression inlets at angle of attack | 1 |
| 18 | 2 | |
| 19 | 4 | |
| 20 | Calculation of the flow field in supersonic mixed-compression inlets at angle of attack using the three-dimensional method of characteristics with discrete shock wave fitting | 4 |
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.