L. H. Smith
- Aerospace Engineering top 1%
- Computational Mechanics top 2%
- Mechanical Engineering top 5%
- Global and Planetary Change top 10%
- Fluid Flow and Transfer Processes top 10%
- Topics
- Turbomachinery Performance and Optimization (18 papers)Refrigeration and Air Conditioning Technologies (12 papers)Fluid Dynamics and Turbulent Flows (6 papers)
- Partner nations
- United States
In The Last Decade
L. H. Smith
25 papers receiving 958 citations
Peers
Comparison fields: 5 of 37
- Aerospace Engineering 936
- Computational Mechanics 629
- Mechanical Engineering 442
- Global and Planetary Change 258
- Fluid Flow and Transfer Processes 61
Countries citing papers authored by L. H. Smith
This map shows the geographic impact of L. H. Smith'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 L. H. Smith with the expected number of citations based on a country's size and research output (numbers larger than one mean the country cites L. H. Smith more than expected).
Fields of papers citing papers by L. H. Smith
This network shows the impact of papers produced by L. H. Smith. 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 L. H. Smith. The network helps show where L. H. Smith may publish in the future.
Co-authorship network of co-authors of L. H. Smith
This figure shows the co-authorship network connecting the top 25 collaborators of L. H. Smith. A scholar is included among the top collaborators of L. H. Smith 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 L. H. Smith. L. H. Smith is excluded from the visualization to improve readability, since they are connected to all nodes in the network.
All Works
| # | Work | Indexed citations |
|---|---|---|
| 1 | The development of a double headshaft, moving chain diffuser: design, installation and performance. | 1 |
| 2 | 31 | |
| 3 | 3 | |
| 4 | 14 | |
| 5 | 258 | |
| 6 | 11 | |
| 7 | 13 | |
| 8 | 1 | |
| 9 | 276 | |
| 10 | LOSS SOURCES AND MAGNITUDE IN AXIAL-FLOW COMPRESSORS | 3 |
| 11 | 1 | |
| 12 | Experimental evaluation of outer case blowing or bleeding of single stage axial flow compressor. Part I - Design of rotor and bleeding and blowing configurations | 3 |
| 13 | 94 | |
| 14 | 112 | |
| 15 | 5 | |
| 16 | 91 | |
| 17 | 1 | |
| 18 | 7 | |
| 19 | 17 | |
| 20 | Three-dimensional flow in axial-flow turbomachinery | 4 |
About L. H. Smith
L. H. Smith is a scholar working on Aerospace Engineering, Computational Mechanics and Mechanical Engineering, having authored 27 papers that have together received 1.1k indexed citations. Recurring topics across this work include Turbomachinery Performance and Optimization (18 papers), Refrigeration and Air Conditioning Technologies (12 papers) and Fluid Dynamics and Turbulent Flows (6 papers). The work is most often cited by research in Aerospace Engineering (936 citations), Computational Mechanics (629 citations) and Global and Planetary Change (258 citations). L. H. Smith has collaborated with scholars based in United States. Frequent co-authors include C. C. Koch, Hsuan Yeh, D. C. Wisler, J. P. Gostelow and Cheng Rong. Their work appears in journals such as Science, Journal of Fluids Engineering and Journal of Propulsion and Power.
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.