Allan Paull
- Computational Mechanics top 2%
- Aerospace Engineering top 2%
- Applied Mathematics top 2%
- Control and Systems Engineering
- Fluid Flow and Transfer Processes
- Co-authors
- Michael K. SmartNeal HassRoger L. KimmelDavid AdamczakRussell BoyceD. J. MeeDavid Van WieSook-Ying Ho
- Topics
- Computational Fluid Dynamics and Aerodynamics (21 papers)Gas Dynamics and Kinetic Theory (16 papers)Rocket and propulsion systems research (14 papers)
- Partner nations
- AustraliaUnited StatesGermany
In The Last Decade
Allan Paull
30 papers receiving 692 citations
Peers
Comparison fields: 5 of 43
- Computational Mechanics 613
- Aerospace Engineering 462
- Applied Mathematics 330
- Control and Systems Engineering 26
- Fluid Flow and Transfer Processes 24
Countries citing papers authored by Allan Paull
This map shows the geographic impact of Allan Paull'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 Allan Paull with the expected number of citations based on a country's size and research output (numbers larger than one mean the country cites Allan Paull more than expected).
Fields of papers citing papers by Allan Paull
This network shows the impact of papers produced by Allan Paull. 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 Allan Paull. The network helps show where Allan Paull may publish in the future.
Co-authorship network of co-authors of Allan Paull
This figure shows the co-authorship network connecting the top 25 collaborators of Allan Paull. A scholar is included among the top collaborators of Allan Paull 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 Allan Paull. Allan Paull 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 | 0 | |
| 3 | 36 | |
| 4 | 27 | |
| 5 | 21 | |
| 6 | 27 | |
| 7 | 12 | |
| 8 | 6 | |
| 9 | 17 | |
| 10 | 1 | |
| 11 | 242 | |
| 12 | 18 | |
| 13 | 4 | |
| 14 | Ground Testing of the HyShot Supersonic Combustion Flight Experiment in HEG and Comparison with Flight Data (AIAA 2004–3345) | 9 |
| 15 | 2 | |
| 16 | 65 | |
| 17 | 14 | |
| 18 | 6 | |
| 19 | 1 | |
| 20 | 1 |
About Allan Paull
Allan Paull is a scholar working on Applied Mathematics, Computational Mechanics and Aerospace Engineering, having authored 31 papers that have together received 729 indexed citations. Recurring topics across this work include Computational Fluid Dynamics and Aerodynamics (21 papers), Gas Dynamics and Kinetic Theory (16 papers) and Rocket and propulsion systems research (14 papers). The work is most often cited by research in Applied Mathematics (330 citations), Computational Mechanics (613 citations) and Aerospace Engineering (462 citations). Allan Paull has collaborated with scholars based in Australia, United States and Germany. Frequent co-authors include Michael K. Smart, Neal Hass, Roger L. Kimmel, David Adamczak, Russell Boyce, D. J. Mee, David Van Wie, Sook-Ying Ho, Timothy J. McIntyre and Thomas J. Juliano. Their work appears in journals such as AIAA Journal, Journal of Propulsion and Power and Aerospace Science and Technology.
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.