World's Best Scientists 2026 revealed!

D-Index & Metrics

Mechanical and Aerospace Engineering

D-Index
61
Citations
11066
World Ranking
668
National Ranking
289

Overview

Ronald Scott Bunker is affiliated with General Electric in the United States. Their professional activities are centered within this organization and region.

There are no records of recent papers published by Ronald Scott Bunker. Likewise, there are no frequent co-authors or recurring publication venues associated with their work in the available data.

Their research focus does not list any specific main fields of study, subfields, or main topics. Similarly, there is no information on book publications or awards received.

While the specific details of their scientific output and collaborations are not documented here, their connection to General Electric suggests involvement in applied or industrial research fields that align with GE's business areas.

Best Publications

  • A review of shaped hole turbine film-cooling technology

    Ronald S. Bunker

  • Axial Turbine Blade Tips: Function, Design, and Durability

    Ronald S. Bunker

  • Effect of Trench Width and Depth on Film Cooling From Cylindrical Holes Embedded in Trenches

    Yiping Lu;Alok Dhungel;Srinath V. Ekkad;Ronald S. Bunker

  • Gas Turbine Heat Transfer: Ten Remaining Hot Gas Path Challenges

    Ronald S. Bunker

  • Local Heat Transfer in Internally Cooled Turbine Airfoil Leading Edge Regions: Part II—Impingement Cooling With Film Coolant Extraction

    D. E. Metzger;R. S. Bunker

  • Film cooled wall with chevron-shaped cooling holes

    Lee Ching-Pang;Ronald Scott Bunker;Steven Robert Brassfield

  • A Review of Turbine Blade Tip Heat Transfer

    Ronald S. Bunker

  • METHOD FOR IMPROVING COOLING EFFECT OF GASEOUS COOLING MEDIUM FLOW AND RELEVANT PRODUCT

    Bunker Ronald Scott;Bailey Jeremy Clyde;Lee Ching-Pang;Abuaf Nesim

  • Film Cooling Effectiveness Due to Discrete Holes Within a Transverse Surface Slot

    Ronald S. Bunker

  • Heat Transfer and Flow on the First Stage Blade Tip of a Power Generation Gas Turbine: Part 1 — Experimental Results

    Ronald S. Bunker;Jeremy C. Bailey;Ali A. Ameri

  • Cavity Heat Transfer on a Transverse Grooved Wall in a Narrow Flow Channel

    D. E. Metzger;R. S. Bunker;M. K. Chyu

  • Heat Transfer and Flow on the First Stage Blade Tip of a Power Generation Gas Turbine: Part 2 — Simulation Results

    A. A. Ameri;R. S. Bunker

  • Film cooled wall

    Ching-Pang Lee;Ronald Scott Bunker;Nesim Abuaf

  • Turbine stage with scalloped surface platform

    Anna Tam;Ching-Pang Lee;Kevin Richard Kirtley;Ronald Scott Bunker

  • Turbine airfoil with double shell outer wall

    Ronald S. Bunker;Thomas T. Wallace

  • Heat Transfer Coefficients on the Squealer Tip and Near-Tip Regions of a Gas Turbine Blade With Single or Double Squealer

    Jae Su Kwak;Jaeyong Ahn;Je-Chin Han;C. Pang Lee

  • Film cooled blade tip

    Ronald Scott Bunker

  • Cooling for double-wall structures

    Ronald Scott Bunker

  • The Effects of Manufacturing Tolerances on Gas Turbine Cooling

    Ronald S. Bunker

  • Effect of Squealer Geometry Arrangement on a Gas Turbine Blade Tip Heat Transfer

    Gm Salam Azad;Je-Chin Han;Ronald S. Bunker;C. Pang Lee

  • Hot gas path component with mesh and impingement cooling

    Ronald Scott Bunker;Ching-Pang Lee

Frequent Co-Authors

Ching-Pang Lee
Ching-Pang Lee Independent Scientist / Consultant, US
Srinath V. Ekkad
Srinath V. Ekkad North Carolina State University
Melvin Robert Jackson
Melvin Robert Jackson General Electric (United States)
Je-Chin Han
Je-Chin Han Texas A&M University
David G. Bogard
David G. Bogard The University of Texas at Austin
Sumanta Acharya
Sumanta Acharya Illinois Institute of Technology
Minking K. Chyu
Minking K. Chyu University of Pittsburgh

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