R. E. Sheer

496 total citations
35 papers, 353 citations indexed

About

R. E. Sheer is a scholar working on Computational Mechanics, Applied Mathematics and Aerospace Engineering. According to data from OpenAlex, R. E. Sheer has authored 35 papers receiving a total of 353 indexed citations (citations by other indexed papers that have themselves been cited), including 25 papers in Computational Mechanics, 18 papers in Applied Mathematics and 18 papers in Aerospace Engineering. Recurrent topics in R. E. Sheer's work include Gas Dynamics and Kinetic Theory (18 papers), Fluid Dynamics and Turbulent Flows (15 papers) and Computational Fluid Dynamics and Aerodynamics (14 papers). R. E. Sheer is often cited by papers focused on Gas Dynamics and Kinetic Theory (18 papers), Fluid Dynamics and Turbulent Flows (15 papers) and Computational Fluid Dynamics and Aerodynamics (14 papers). R. E. Sheer collaborates with scholars based in United States, Switzerland and Germany. R. E. Sheer's co-authors include H. T. Nagamatsu, John A. Weil, Joseph Workman, D. M. Kercher, R. M. C. So, Leik Myrabo, D. C. Wisler and Yoshio Yoshioka and has published in prestigious journals such as Journal of Fluid Mechanics, AIAA Journal and The Physics of Fluids.

In The Last Decade

R. E. Sheer

34 papers receiving 320 citations

Peers — A (Enhanced Table)

Peers by citation overlap · career bar shows stage (early→late) cites · hero ref

Name	h						Papers	Cites
R. E. Sheer United States	12	247	178	176	55	31	35	353
G.N. Patterson Canada	5	143 0.6×	112 0.6×	144 0.8×	37 0.7×	29 0.9×	11	298
E. P. Bartlett United States	10	188 0.8×	206 1.2×	292 1.7×	36 0.7×	31 1.0×	20	414
Stephen H Maslen United States	9	215 0.9×	159 0.9×	158 0.9×	27 0.5×	45 1.5×	22	378
V. Zakkay United States	14	498 2.0×	293 1.6×	188 1.1×	80 1.5×	44 1.4×	62	627
D. M. Kuehn United States	6	588 2.4×	354 2.0×	223 1.3×	62 1.1×	14 0.5×	12	678
A. J. Laderman United States	12	260 1.1×	195 1.1×	98 0.6×	76 1.4×	8 0.3×	49	402
Donald J. Carlson Finland	5	235 1.0×	203 1.1×	100 0.6×	157 2.9×	13 0.4×	10	384
Clark H. Lewis United States	12	291 1.2×	185 1.0×	288 1.6×	62 1.1×	10 0.3×	59	388
G. Moretti United States	12	463 1.9×	178 1.0×	233 1.3×	15 0.3×	33 1.1×	35	570
Hartmut H. Legner United States	10	307 1.2×	188 1.1×	79 0.4×	66 1.2×	70 2.3×	36	440

Countries citing papers authored by R. E. Sheer

Since Specialization

Citations

This map shows the geographic impact of R. E. Sheer'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 R. E. Sheer with the expected number of citations based on a country's size and research output (numbers larger than one mean the country cites R. E. Sheer more than expected).

Fields of papers citing papers by R. E. Sheer

Since Specialization

Physical SciencesHealth SciencesLife SciencesSocial Sciences

This network shows the impact of papers produced by R. E. Sheer. 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 R. E. Sheer. The network helps show where R. E. Sheer may publish in the future.

Co-authorship network of co-authors of R. E. Sheer

This figure shows the co-authorship network connecting the top 25 collaborators of R. E. Sheer. A scholar is included among the top collaborators of R. E. Sheer 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 R. E. Sheer. R. E. Sheer is excluded from the visualization to improve readability, since they are connected to all nodes in the network.

All Works

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20 of 20 papers shown

Nagamatsu, H. T., et al.. (1999). Combustion-driven hypersonic shock tunnel MHD results relevant to advanced propulsion concepts. 2 indexed citations

Kercher, D. M., R. E. Sheer, & R. M. C. So. (1983). Short Duration Heat Transfer Studies at High Free-Stream Temperatures. Journal of Engineering for Power. 105(1). 156–166. 9 indexed citations

Nagamatsu, H. T., et al.. (1983). Application of arc-interruption fundamentals to nozzles for puffer interrupters. Final report. OSTI OAI (U.S. Department of Energy Office of Scientific and Technical Information). 1 indexed citations

Kercher, D. M., R. E. Sheer, & R. M. C. So. (1982). Short Duration Heat Transfer Studies at High Free-Stream Temperatures. 1 indexed citations

Nagamatsu, H. T., et al.. (1980). Fundamental investigation of ARC interruption in gas flows. 15 indexed citations

Nagamatsu, H. T. & R. E. Sheer. (1973). Subsonic and supersonic jets and supersonic suppressor characteristics. NASA STI Repository (National Aeronautics and Space Administration). 4 indexed citations

Nagamatsu, H. T., et al.. (1972). Mean and fluctuating velocity contours and acoustic characteristics of subsonic and supersonic jets. NASA STI Repository (National Aeronautics and Space Administration). 3 indexed citations

Nagamatsu, H. T., et al.. (1972). Subsonic and supersonic jet flow and acoustic characteristics and supersonic suppressors. NASA Technical Reports Server (NASA). 2 indexed citations

Nagamatsu, H. T. & R. E. Sheer. (1972). Flow, thrust, and acoustic characteristics of 50 tubes with 50 shrouds supersonic jet noise suppressor. 3 indexed citations

10.

Nagamatsu, H. T., et al.. (1970). Flow and acoustic characteristics of subsonic and supersonic jets from convergent nozzle. NASA Technical Reports Server (NASA). 6 indexed citations

11.

Nagamatsu, H. T. & R. E. Sheer. (1970). Heat transfer on a flat plate in continuum to rarefied hypersonic flows at Mach numbers of 19.2 and 25.4. NASA Technical Reports Server (NASA). 1 indexed citations

12.

Nagamatsu, H. T., D. C. Wisler, & R. E. Sheer. (1969). Circumferential Nonuniform Heating during Transition on a Slender Cone at Hypersonic Mach Numbers. The Physics of Fluids. 12(5). 959–966. 2 indexed citations

13.

Nagamatsu, H. T., et al.. (1967). Hypersonic laminar boundary-layer transition on 8-foot-long, 10 deg cone, M sub 1 equals 9.1-16.. AIAA Journal. 5(7). 1245–1252. 23 indexed citations

14.

Nagamatsu, H. T., et al.. (1966). Roughness, bluntness, and angle-of-attack effects on hypersonic boundary-layer transition. Journal of Fluid Mechanics. 24(1). 1–31. 16 indexed citations

15.

Nagamatsu, H. T., et al.. (1965). Transition of Hypersonic Boundary Layer. The Physics of Fluids. 8(2). 211–221. 6 indexed citations

16.

Nagamatsu, H. T. & R. E. Sheer. (1964). Vibrational relaxation and recombination of nitrogen and air in hypersonic nozzle flows. 1 indexed citations

17.

Nagamatsu, H. T., R. E. Sheer, & John A. Weil. (1963). RAREFIED HIGH-TEMPERATURE, ULTRAHIGH MACH NUMBER SLIP FLOW OVER A SHARP FLAT PLATE,. Defense Technical Information Center (DTIC). 3 indexed citations

18.

Nagamatsu, H. T., Joseph Workman, & R. E. Sheer. (1961). Hypersonic Nozzle Expansion of Air With Atom Recombination Present. Journal of the aerospace sciences. 28(11). 833–837. 15 indexed citations

19.

Nagamatsu, H. T., et al.. (1960). Real Gas Effects in Flow over Blunt Bodies at Hypersonic Speeds. Journal of the aerospace sciences. 27(4). 241–251. 26 indexed citations

20.

Nagamatsu, H. T. & R. E. Sheer. (1960). Hypersonic Shock Wave-Boundary Layer Interaction and Leading Edge Slip. ARS journal. 30(5). 454–462. 21 indexed citations

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.

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