P. M. Siemers
About
In The Last Decade
P. M. Siemers
42 papers receiving 344 citations
Peers
Comparison fields: 5 of 34
- Aerospace Engineering 303
- Applied Mathematics 139
- Astronomy and Astrophysics 106
- Computational Mechanics 95
- Artificial Intelligence 63
Countries citing papers authored by P. M. Siemers
This map shows the geographic impact of P. M. Siemers'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 P. M. Siemers with the expected number of citations based on a country's size and research output (numbers larger than one mean the country cites P. M. Siemers more than expected).
Fields of papers citing papers by P. M. Siemers
This network shows the impact of papers produced by P. M. Siemers. 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 P. M. Siemers. The network helps show where P. M. Siemers may publish in the future.
Co-authorship network of co-authors of P. M. Siemers
This figure shows the co-authorship network connecting the top 25 collaborators of P. M. Siemers. A scholar is included among the top collaborators of P. M. Siemers 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 P. M. Siemers. P. M. Siemers is excluded from the visualization to improve readability, since they are connected to all nodes in the network.
All Works
| # | Work | Indexed citations |
|---|---|---|
| 1 | 1 | |
| 2 | Mars Entry Atmospheric Data System Modeling, Calibration, and Error Analysis | 5 |
| 3 | 10 | |
| 4 | Wind-tunnel investigation of a flush airdata system at Mach numbers from 0.7 to 1.4 | 12 |
| 5 | Research at the earth's edge | 1 |
| 6 | 7 | |
| 7 | Aeroassist Flight Experiment (AFE) | 1 |
| 8 | The Aeroassist Flight Experiment | 12 |
| 9 | Pressure distributions obtained on a 0.10-scale model of the Space Shuttle Orbiter's forebody in the Ames Unitary Plan Wind Tunnel | 1 |
| 10 | Pressure distributions obtained on a 0.10-scale model of the space shuttle Orbiter's forebody in the AEDC 16T propulsion wind tunnel | 2 |
| 11 | 4 | |
| 12 | 1 | |
| 13 | Shuttle flight pressure instrumentation: Experience and lessons for the future | 6 |
| 14 | Pressure distributions obtained on a 0.04-scale and 0.02-scale model of the Space Shuttle Orbiter's forward fuselage in the Langley continuous flow hypersonic tunnel | 3 |
| 15 | Pressure distributions on a 0.04-scale model of the Space Shuttle Orbiter's forward fuselage in the Langley unitary plan wind tunnel | 3 |
| 16 | Pressure distributions obtained on a 0.04-scale and 0.02-scale model of the Space Shuttle Orbiter's forward fuselage in the Langley 20-inch Mach 6 air tunnel | 1 |
| 17 | Subsonic tests of an all-flush-pressure-orifice air data system | 14 |
| 18 | Wind tunnel investigation of an all flush orifice air data system for a large subsonic aircraft. [conducted in a Langley 8 foot transonic pressure tunnel | 5 |
| 19 | Shuttle Entry Air Data System | 6 |
| 20 | 9 |
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.