D. C. Rabe

735 total citations
39 papers, 589 citations indexed

About

D. C. Rabe is a scholar working on Aerospace Engineering, Computational Mechanics and Mechanical Engineering. According to data from OpenAlex, D. C. Rabe has authored 39 papers receiving a total of 589 indexed citations (citations by other indexed papers that have themselves been cited), including 29 papers in Aerospace Engineering, 22 papers in Computational Mechanics and 18 papers in Mechanical Engineering. Recurrent topics in D. C. Rabe's work include Turbomachinery Performance and Optimization (27 papers), Fluid Dynamics and Turbulent Flows (15 papers) and Refrigeration and Air Conditioning Technologies (11 papers). D. C. Rabe is often cited by papers focused on Turbomachinery Performance and Optimization (27 papers), Fluid Dynamics and Turbulent Flows (15 papers) and Refrigeration and Air Conditioning Technologies (11 papers). D. C. Rabe collaborates with scholars based in United States. D. C. Rabe's co-authors include Chunill Hah, A. R. Wadia, Paul King, Timothy J. Sullivan, Rolf Sondergaard, Marc D. Polanka, Christopher B. Lorence, Walter F. O’Brien, A. Bölcs and Larry Goss and has published in prestigious journals such as Review of Scientific Instruments, Journal of Propulsion and Power and Journal of Turbomachinery.

In The Last Decade

D. C. Rabe

39 papers receiving 531 citations

Peers — A (Enhanced Table)

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

Name	h						Papers	Cites
D. C. Rabe United States	14	519	350	308	41	28	39	589
Jean-François Brouckaert Belgium	11	228 0.4×	159 0.5×	127 0.4×	29 0.7×	94 3.4×	25	339
Reinhard Niehuis Germany	16	1.1k 2.1×	875 2.5×	518 1.7×	17 0.4×	58 2.1×	153	1.2k
Guoqiang Yue China	13	339 0.7×	255 0.7×	279 0.9×	10 0.2×	11 0.4×	51	427
Masato FURUKAWA Japan	16	711 1.4×	565 1.6×	443 1.4×	24 0.6×	34 1.2×	85	833
Tomoki Kawakubo Japan	11	233 0.4×	163 0.5×	173 0.6×	8 0.2×	20 0.7×	19	308
Jun Su Park South Korea	13	311 0.6×	281 0.8×	396 1.3×	27 0.7×	27 1.0×	44	503
Jae Su Kwak South Korea	21	1.1k 2.2×	1.0k 3.0×	1.2k 4.0×	24 0.6×	68 2.4×	82	1.4k
Yuting Jiang China	17	432 0.8×	355 1.0×	462 1.5×	16 0.4×	21 0.8×	49	621
Ce Yang China	16	565 1.1×	441 1.3×	362 1.2×	34 0.8×	44 1.6×	91	762
Kam Chana United Kingdom	14	508 1.0×	491 1.4×	340 1.1×	17 0.4×	60 2.1×	52	664

Countries citing papers authored by D. C. Rabe

Since Specialization

Citations

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

Fields of papers citing papers by D. C. Rabe

Since Specialization

Physical SciencesHealth SciencesLife SciencesSocial Sciences

This network shows the impact of papers produced by D. C. Rabe. 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 D. C. Rabe. The network helps show where D. C. Rabe may publish in the future.

Co-authorship network of co-authors of D. C. Rabe

This figure shows the co-authorship network connecting the top 25 collaborators of D. C. Rabe. A scholar is included among the top collaborators of D. C. Rabe 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 D. C. Rabe. D. C. Rabe 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

Hah, Chunill, et al.. (2015). Investigation of Unsteady Flow Interaction Between an Ultra-Compact Inlet and a Transonic Fan. NASA Technical Reports Server (NASA). 2 indexed citations

O’Brien, Walter F., et al.. (2010). Predicting Separation and Transitional Flow in Turbine Blades at Low Reynolds Numbers—Part I: Development of Prediction Methodology. Journal of Turbomachinery. 133(3). 23 indexed citations

O’Brien, Walter F., et al.. (2009). A Mixing Plane Model Investigation of Separation and Transitional Flow at Low Reynolds Numbers in a Multistage Low Pressure Turbine. 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. 4 indexed citations

Hah, Chunill, D. C. Rabe, & A. R. Wadia. (2004). Role of Tip-Leakage Vortices and Passage Shock in Stall Inception in a Swept Transonic Compressor Rotor. 545–555. 71 indexed citations

Rabe, D. C., et al.. (2004). Experimental and Numerical Study of Stall Flutter in a Transonic Low-Aspect Ratio Fan Blisk. Journal of Turbomachinery. 126(1). 166–174. 44 indexed citations

O’Brien, Walter F., et al.. (2003). Multi-Stage Fan and Compressor Transfer of Inlet Total Pressure Distortion with Emphasis on High Cycle Fatigue. 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. 1 indexed citations

Rabe, D. C., et al.. (2003). Experimental and Numerical Study of Stall Flutter in a Transonic Low-Aspect Ratio Fan Blisk. 339–348. 7 indexed citations

Wadia, A. R., et al.. (2002). Forward Swept Rotor Studies in Multistage Fans With Inlet Distortion. 11–21. 11 indexed citations

Rabe, D. C. & Chunill Hah. (2002). Application of Casing Circumferential Grooves for Improved Stall Margin in a Transonic Axial Compressor. 76 indexed citations

10.

Kenyon, James Andrew, D. C. Rabe, & Sanford Fleeter. (1999). Aerodynamic Effects on Blade Vibratory Stress Variations. Journal of Propulsion and Power. 15(5). 675–680. 9 indexed citations

11.

Kenyon, James Andrew, D. C. Rabe, & Sanford Fleeter. (1998). Aerodynamic effects on blade vibratory stress variations. 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. 3 indexed citations

12.

King, Paul, et al.. (1998). Experimental and Computational Investigation of Stepped Tip Gap Effects on the Flowfield of a Transonic Axial-Flow Compressor Rotor. Volume 1: Turbomachinery. 12 indexed citations

13.

Hah, Chunill, D. C. Rabe, Timothy J. Sullivan, & A. R. Wadia. (1998). Effects of Inlet Distortion on the Flow Field in a Transonic Compressor Rotor. Journal of Turbomachinery. 120(2). 233–246. 57 indexed citations

14.

King, Paul, et al.. (1997). Experimental Investigation of Stepped Tip Gap Effects on the Performance of a Transonic Axial-Flow Compressor Rotor. Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery. 27 indexed citations

15.

Rabe, D. C., et al.. (1995). Influence of inlet distortion on transonic compressor blade loading. 31st Joint Propulsion Conference and Exhibit. 24 indexed citations

16.

Rabe, D. C., et al.. (1995). Pressure-Sensitive Paint Investigation for Turbomachinery Application. Volume 1: Turbomachinery. 5 indexed citations

17.

Cybyk, Bohdan, et al.. (1995). Characterization of the first-stage rotor in a two-stage transonic compressor. 31st Joint Propulsion Conference and Exhibit. 9 indexed citations

18.

Rabe, D. C., Arthur J. Wennerstrom, & W. F. O’Brien. (1988). Characterization of Shock Wave–Endwall Boundary Layer Interactions in a Transonic Compressor Rotor. Journal of Turbomachinery. 110(3). 386–392. 5 indexed citations

19.

Rabe, D. C., et al.. (1978). Heat pipe mirrors for high power lasers. 4 indexed citations

20.

Olson, Robert, et al.. (1978). High-power CO2 laser-beam monitor. Review of Scientific Instruments. 49(6). 778–781. 1 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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