H. W. Carlson
- Computational Mechanics top 2%
- Aerospace Engineering top 2%
- Environmental Engineering top 10%
- Applied Mathematics top 5%
- Global and Planetary Change top 10%
- Co-authors
- Robert J. MackDomenic J. MaglieriDavid S. MillerJulio ChuHarvey H. HubbardNorman F. Smith
- Topics
- Computational Fluid Dynamics and Aerodynamics (50 papers)Fluid Dynamics and Turbulent Flows (20 papers)Aerospace and Aviation Technology (16 papers)
- Partner nations
- United States
In The Last Decade
H. W. Carlson
60 papers receiving 669 citations
Peers
Comparison fields: 5 of 48
- Computational Mechanics 566
- Aerospace Engineering 558
- Environmental Engineering 112
- Applied Mathematics 104
- Global and Planetary Change 104
Countries citing papers authored by H. W. Carlson
This map shows the geographic impact of H. W. Carlson'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 H. W. Carlson with the expected number of citations based on a country's size and research output (numbers larger than one mean the country cites H. W. Carlson more than expected).
Fields of papers citing papers by H. W. Carlson
This network shows the impact of papers produced by H. W. Carlson. 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 H. W. Carlson. The network helps show where H. W. Carlson may publish in the future.
Co-authorship network of co-authors of H. W. Carlson
This figure shows the co-authorship network connecting the top 25 collaborators of H. W. Carlson. A scholar is included among the top collaborators of H. W. Carlson 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 H. W. Carlson. H. W. Carlson is excluded from the visualization to improve readability, since they are connected to all nodes in the network.
All Works
| # | Work | Indexed citations |
|---|---|---|
| 1 | 2 | |
| 2 | Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application to optimization | 10 |
| 3 | A modification to linearized theory for prediction of pressure loadings on lifting surfaces at high supersonic Mach numbers and large angles of attack | 1 |
| 4 | Estimation of Attainable Leading-Edge Thrust for Wings at Subsonic and Supersonic Speeds | 41 |
| 5 | 2 | |
| 6 | 4 | |
| 7 | Estimation of leading-edge thrust for supersonic wings of arbitrary planform | 20 |
| 8 | A wind-tunnel study of the applicability of far-field sonic-boom theory to the space shuttle orbiter | 3 |
| 9 | Numerical methods for the design and analysis of wings at supersonic speeds | 43 |
| 10 | Application of sonic-boom minimization concepts in supersonic transport design | 25 |
| 11 | Some Notes on the Present Status of Sonic Boom Prediction and Minimization Research | 0 |
| 12 | Wind-tunnel investigation of sonic-boom characteristics of two simple wing models at Mach numbers from 2.3 to 4.63 | 6 |
| 13 | A study of the application of heat or force fields to the sonic-boom-minimization problem | 21 |
| 14 | Experimental and analytic research on sonic boom generation at NASA | 9 |
| 15 | 4 | |
| 16 | An Investigation of Some Aspects of the Sonic Boom by Means of Wind-Tunnel Measurements of Pressures About Several Bodies at a Mach Number of 2.01 | 14 |
| 17 | Measurement of Static Forces on Internally Carried Bombs of Three Fineness Ratios in Flow Field of a Swept-wing Fighter-bomber Configuration at a Mach Number of 1.61 with Illustrative Drop Path Calculations | 1 |
| 18 | The Origin and Distribution of Supersonic Store Interference From Measurement of Individual Forces on Several Wing-fuselage-store Configurations. Ii - Swept-wing Heavy-bomber Configuration With Large Store Nacelle . Lateral Forces and Pitching Moments, Mach Number, 1.61 | 0 |
| 19 | CALCULATION OF DEPTH OF FREEZING AND THAWING UNDER PAVEMENTS | 3 |
| 20 | CALCULATION OF DEPTH OF THAW IN FROZEN GROUND | 29 |
About H. W. Carlson
H. W. Carlson is a scholar working on Computational Mechanics, Aerospace Engineering and Environmental Engineering, having authored 68 papers that have together received 786 indexed citations. Recurring topics across this work include Computational Fluid Dynamics and Aerodynamics (50 papers), Fluid Dynamics and Turbulent Flows (20 papers) and Aerospace and Aviation Technology (16 papers). The work is most often cited by research in Computational Mechanics (566 citations), Aerospace Engineering (558 citations) and Applied Mathematics (104 citations). H. W. Carlson has collaborated with scholars based in United States. Frequent co-authors include Robert J. Mack, Domenic J. Maglieri, David S. Miller, Julio Chu, Harvey H. Hubbard and Norman F. Smith. Their work appears in journals such as The Journal of the Acoustical Society of America, Journal of Aircraft and NASSP.
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.