D. O. O’Dowd

510 citations

13 papers · 447 indexed · h-index 9

Co-authors: L. He Q. Zhang Phil Ligrani M. L. G. Oldfield Andrew P. S. Wheeler S. Friedrichs Phillip M. Ligrani Aaron R. Byerley
Topics: Turbomachinery Performance and Optimization (12 papers)Heat Transfer Mechanisms (9 papers)Fluid Dynamics and Turbulent Flows (6 papers)
Cited by: Computational Mechanics Aerospace Engineering Mechanical Engineering
Journals: Journal of TurbomachineryVolume 4: Heat Transfer, Parts A and BDefense Technical Information Center (DTIC)
Partner nations: United Kingdom United States China

In The Last Decade

D. O. O’Dowd

13 papers receiving 440 citations

Peers

Countries citing papers authored by D. O. O’Dowd

Since Specialization

Citations

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

Fields of papers citing papers by D. O. O’Dowd

Since Specialization

Physical SciencesHealth SciencesLife SciencesSocial Sciences

This network shows the impact of papers produced by D. O. O’Dowd. 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. O. O’Dowd. The network helps show where D. O. O’Dowd may publish in the future.

Co-authorship network of co-authors of D. O. O’Dowd

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

All Works

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13 of 13 papers shown

#	Work	Indexed citations
1	Computational Aid to AEDsys for Designing a Variable-Area Gas Turbine Nozzle 2018 ·D. O. O’Dowd,Aaron R. Byerley	1
2	Exploring GasTurb 12 for Supplementary Use on an Introductory Propulsion Design Project 2017 ·Aaron R. Byerley,(unknown),D. O. O’Dowd	7
3	Aerothermal Performance of a Cooled Winglet at Engine Representative Mach and Reynolds Numbers 2012 ·Journal of Turbomachinery ·D. O. O’Dowd,(unknown),L. He,(unknown),(unknown)	35
4	Aerothermal Performance of a Winglet at Engine Representative Mach and Reynolds Numbers 2011 ·Journal of Turbomachinery ·D. O. O’Dowd,Q. Zhang,L. He,M. L. G. Oldfield,Phillip M. Ligrani,(unknown),(unknown)	45
5	Overtip Shock Wave Structure and Its Impact on Turbine Blade Tip Heat Transfer 2011 ·Journal of Turbomachinery ·Q. Zhang,D. O. O’Dowd,L. He,Andrew P. S. Wheeler,Phil Ligrani,(unknown)	106
6	Transonic Turbine Blade Tip Aerothermal Performance With Different Tip Gaps—Part I: Tip Heat Transfer 2011 ·Journal of Turbomachinery ·Q. Zhang,D. O. O’Dowd,L. He,M. L. G. Oldfield,Phil Ligrani	93
7	Aero-Thermal Performance of a Cooled Winglet at Engine Representative Mach and Reynolds Numbers 2011 ·D. O. O’Dowd,Q. Zhang,L. He,(unknown),(unknown)	11
8	Aero-Thermal Performance of a Winglet at Engine Representative Mach and Reynolds Numbers 2010 ·Volume 4: Heat Transfer, Parts A and B ·D. O. O’Dowd,Q. Zhang,L. He,M. L. G. Oldfield,Phil Ligrani,(unknown),(unknown)	55
9	Transonic Turbine Blade Tip Aero-Thermal Performance With Different Tip Gaps: Part II—Tip Aerodynamic Loss 2010 ·Volume 4: Heat Transfer, Parts A and B ·D. O. O’Dowd,Q. Zhang,(unknown),L. He,Phil Ligrani	19
10	Comparison of Heat Transfer Measurement Techniques on a Transonic Turbine Blade Tip 2010 ·Journal of Turbomachinery ·D. O. O’Dowd,Q. Zhang,L. He,Phil Ligrani,S. Friedrichs	55
11	Transonic Turbine Blade Tip Aero-Thermal Performance With Different Tip Gaps: Part I—Tip Heat Transfer 2010 ·Volume 4: Heat Transfer, Parts A and B ·Q. Zhang,D. O. O’Dowd,L. He,M. L. G. Oldfield,Phil Ligrani	13
12	Comparison of Heat Transfer Measurement Techniques on a Transonic Turbine Blade Tip 2009 ·D. O. O’Dowd,Qiang Zhang,Phil Ligrani,L. He,S. Friedrichs	6
13	An Example for Integrated Gas Turbine Engine Testing and Analysis Using Modeling and Simulation 2006 ·Defense Technical Information Center (DTIC) ·Milt Davis,(unknown),(unknown),D. O. O’Dowd	1

About D. O. O’Dowd

D. O. O’Dowd is a scholar working on Aerospace Engineering, Computational Mechanics and Mechanical Engineering, having authored 13 papers that have together received 447 indexed citations. Recurring topics across this work include Turbomachinery Performance and Optimization (12 papers), Heat Transfer Mechanisms (9 papers) and Fluid Dynamics and Turbulent Flows (6 papers). The work is most often cited by research in Computational Mechanics (371 citations), Aerospace Engineering (418 citations) and Mechanical Engineering (356 citations). D. O. O’Dowd has collaborated with scholars based in United Kingdom, United States and China. Frequent co-authors include L. He, Q. Zhang, Phil Ligrani, M. L. G. Oldfield, Andrew P. S. Wheeler, S. Friedrichs, Phillip M. Ligrani, Aaron R. Byerley, Qiang Zhang and Milt Davis. Their work appears in journals such as Journal of Turbomachinery, Volume 4: Heat Transfer, Parts A and B and Defense Technical Information Center (DTIC).

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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