Countries citing papers authored by I. E. Beckwith
Since
Specialization
Citations
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).
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-authorship network of co-authors of I. E. Beckwith
This figure shows the co-authorship network connecting the top 25 collaborators of I. E. Beckwith.
A scholar is included among the top collaborators of I. E. Beckwith 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 I. E. Beckwith. I. E. Beckwith is excluded from
the visualization to improve readability, since they are connected to all nodes in the network.
Malik, Mujeeb R., et al.. (1987). Experimental and theoretical investigation of boundary-layer instability mechanisms on a swept leading edge at Mach 3.5.2 indexed citations
6.
Beckwith, I. E., et al.. (1985). Nozzle wall roughness effects on free-stream noise and transition in the pilot low-disturbance tunnel. NASA STI/Recon Technical Report N. 85. 34355.6 indexed citations
Beckwith, I. E., et al.. (1981). Gortler vortices and transition in wall boundary layers of two Mach 5 nozzles. NASA STI Repository (National Aeronautics and Space Administration). 81. 31509.14 indexed citations
9.
Beckwith, I. E., et al.. (1981). Effects of a modified leading edge on noise and boundary-layer transition in a rod-wall sound shield at Mach 5. STIN. 81. 22311.1 indexed citations
10.
Beckwith, I. E.. (1981). Comments on settling chamber design for quiet, blowdown wind tunnels. NASA STI Repository (National Aeronautics and Space Administration).6 indexed citations
11.
Beckwith, I. E., et al.. (1980). Noise reduction in a Mach 5 wind tunnel with a rectangular rod-wall sound shield. STIN. 80. 26622.3 indexed citations
Anders, J. B., P. C. Stainback, I. E. Beckwith, & Laurence Keefe. (1975). Sound and fluctuating disturbance measurements in the settling chamber and test section of a small, Mach 5 wind tunnel.7 indexed citations
Beckwith, I. E.. (1970). Recent advances in research on compressible turbulent boundary layers. NASA Technical Reports Server (NASA).10 indexed citations
16.
Beckwith, I. E., Dennis M. Bushnell, & Jcr Hunt. (1970). Finite-difference analysis of the compressible turbulent boundary layer on a blunt swept slab with leading-edge blowing. NASA Technical Reports Server (NASA).4 indexed citations
17.
Beckwith, I. E., Dennis M. Bushnell, & W. D. Harvey. (1969). Fluctuating properties of turbulent boundary layers for Mach numbers up to 9. NASA Technical Reports Server (NASA).17 indexed citations
18.
Beckwith, I. E., Myra Cooper, James Gallagher, & J. J. Jones. (1958). Heat-transfer Measurements on a Concave Hemispherical Nose Shape With Unsteady-flow Effects at Mach Numbers of 1.98 and 4.95.7 indexed citations
19.
Beckwith, I. E.. (1955). Theoretical investigation of laminar heat transfer on yawed infinite cylinders in supersonic flow and a comparison with experimental data. University of North Texas Digital Library (University of North Texas).1 indexed citations
20.
Beckwith, I. E.. (1953). Heat Transfer and Skin Friction by an Integral Method in the Compressible Laminar Boundary Layer With a Streamwise Pressure Gradient. University of North Texas Digital Library (University of North Texas).1 indexed citations
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