I. E. Beckwith
Impact in
- Computational Mechanics top 0.5%
- Fluid Dynamics and Turbulent Flows
- Computational Fluid Dynamics and Aerodynamics
- Combustion and flame dynamics
- Applied Mathematics top 1%
- Gas Dynamics and Kinetic Theory
Papers in
-
- Fluid Dynamics and Turbulent Flows 53
- Computational Fluid Dynamics and Aerodynamics 29
- Radiative Heat Transfer Studies 3
-
- Aerodynamics and Acoustics in Jet Flows 35
- Plasma and Flow Control in Aerodynamics 5
- Co-authors
- Mujeeb R. MalikDennis M. BushnellCharles G. MillerJames GallagherEli ReshotkoM. MâazaStephen WilkinsonJ. M. Kendall
- Journals
- AIAA Journal (8 papers)SAE technical papers on CD-ROM/SAE technical paper series (2 papers)Journal of Fluids Engineering (2 papers)Journal of Aircraft (2 papers)Journal of Spacecraft and Rockets (1 paper)
- Partner nations
- United States
In The Last Decade
I. E. Beckwith
64 papers receiving 1.2k citations
Peers
Comparison fields: 5 of 36
- Computational Mechanics 1.2k
- Applied Mathematics 502
- Aerospace Engineering 727
- Ocean Engineering 150
- Environmental Engineering 128
Countries citing papers authored by I. E. Beckwith
This map shows the geographic impact of I. E. Beckwith'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 I. E. Beckwith with the expected number of citations based on a country's size and research output (numbers larger than one mean the country cites I. E. Beckwith more than expected).
Fields of papers citing papers by I. E. Beckwith
This network shows the impact of papers produced by I. E. Beckwith. 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 I. E. Beckwith. The network helps show where I. E. Beckwith may publish in the future.
Co-authors
The 23 scholars most cited alongside I. E. Beckwith, linked wherever they have co-authored with each other. Click a name or a connecting line to browse the papers they share.
All Works
| # | Work | ||
|---|---|---|---|
| 1 | 1991 | 1 | |
| 2 | 1990 | 112 | |
| 3 | Experimental and theoretical investigation of boundary-layer instability mechanisms on a swept leading edge at Mach 3.5 | 1987 | 2 |
| 4 | 1987 | 2 | |
| 5 | Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel | 1985 | 6 |
| 6 | 1983 | 3 | |
| 7 | Effects of a modified leading edge on noise and boundary-layer transition in a rod-wall sound shield at Mach 5 | 1981 | 1 |
| 8 | Gortler vortices and transition in wall boundary layers of two Mach 5 nozzles | 1981 | 14 |
| 9 | Comments on settling chamber design for quiet, blowdown wind tunnels | 1981 | 6 |
| 10 | Noise reduction in a Mach 5 wind tunnel with a rectangular rod-wall sound shield | 1980 | 3 |
| 11 | 1978 | 13 | |
| 12 | Sound and fluctuating disturbance measurements in the settling chamber and test section of a small, Mach 5 wind tunnel | 1975 | 7 |
| 13 | 1975 | 79 | |
| 14 | Finite-difference analysis of the compressible turbulent boundary layer on a blunt swept slab with leading-edge blowing | 1970 | 4 |
| 15 | Recent advances in research on compressible turbulent boundary layers | 1970 | 10 |
| 16 | Fluctuating properties of turbulent boundary layers for Mach numbers up to 9 | 1969 | 17 |
| 17 | Heat-transfer Measurements on a Concave Hemispherical Nose Shape With Unsteady-flow Effects at Mach Numbers of 1.98 and 4.95 | 1958 | 7 |
| 18 | Compressible laminar boundary layer over a yawed infinite cylinder with heat transfer and arbitrary Prandtl number | 1957 | 65 |
| 19 | Heat Transfer and Skin Friction by an Integral Method in the Compressible Laminar Boundary Layer With a Streamwise Pressure Gradient | 1953 | 1 |
| 20 | The aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section | 1952 | 9 |
About I. E. Beckwith
I. E. Beckwith is a scholar working on Computational Mechanics, Aerospace Engineering, Environmental Engineering, Applied Mathematics and Ocean Engineering, having authored 67 papers that have together received 1.3k indexed citations. Recurring topics across this work include Fluid Dynamics and Turbulent Flows (53 papers), Aerodynamics and Acoustics in Jet Flows (35 papers), Computational Fluid Dynamics and Aerodynamics (29 papers), Wind and Air Flow Studies (14 papers), Particle Dynamics in Fluid Flows (8 papers), Gas Dynamics and Kinetic Theory (8 papers), Plasma and Flow Control in Aerodynamics (5 papers) and Radiative Heat Transfer Studies (3 papers). The work is most often cited by research in Computational Mechanics (1.2k citations), Applied Mathematics (502 citations), Aerospace Engineering (727 citations), Ocean Engineering (150 citations) and Environmental Engineering (128 citations). I. E. Beckwith has collaborated with scholars based in United States. Frequent co-authors include Mujeeb R. Malik, Dennis M. Bushnell, Charles G. Miller, James Gallagher, Eli Reshotko, M. Mâaza, Stephen Wilkinson, J. M. Kendall, P. C. Stainback and J. B. Anders. Their work appears in journals such as AIAA Journal, SAE technical papers on CD-ROM/SAE technical paper series, Journal of Fluids Engineering, Journal of Aircraft and Journal of Spacecraft and Rockets.
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.