Ronald Mathison
Engineering · The Ohio State University
Publications
126
Citations
931
Est. group size
~5
Recurring co-author estimate
Active years
51
Publishing since 1976
Ronald Mathison's research focuses on gas turbine engines, particularly the aerodynamics, heat transfer, and mechanical behavior of turbine blades and disks under realistic engine operating conditions. His work combines experimental facilities (like shock tunnels and rub-force test rigs) with computational modeling to study issues such as blade tip rubbing, film cooling, and endwall contouring for improving turbine efficiency and durability. This research area is relevant to students interested in aerospace/mechanical engineering, propulsion systems, and experimental fluid/thermal engineering.
Publication output has been relatively steady over the last decade with some fluctuation, showing a peak around 2021-2022 and continued activity through 2024-2026.
Generated by claude-sonnet-5 from public bibliographic data · Jul 20, 2026
- Bladed Disk Reduction for Transient Loading in Blade Tip Rubs and Foreign Object Ingestion
Journal of vibration and acoustics · 2026
- The Ohio State University Large-Area Reflected Shock Tunnel: Overview and Characterization
2026
- Performance of Adjoint-Optimized Contoured Endwalls for Multiple Off-Design Purge Flow Rates in Axial Turbines
2025
- Bladed Disk Reduction for Transient Loading Seen in Blade Tip Rubs
2025
- Experimental Identification of Blade Tip Rub Forces at Engine Relevant Temperatures and Speeds
Journal of Engineering for Gas Turbines and Power · 2024
- Adjoint Optimization of Non-Axisymmetric Endwall Contours to Reduce Losses in a High-Pressure Turbine
2024
- Optimizing Thrust Reversal for a Small Turbojet Engine
2024
- A New Experimental Facility for the Study of Blade Tip Rubs at Engine Relevant Temperatures
2024
- NASA HECC Geometry and Performance Review Part 3: A Numerical and Experimental Investigation of Tip Clearance Effects on the Vaneless Diffuser Configuration
2024
- Experimental Identification of Blade Tip Rub Forces at Engine Relevant Temperatures and Speeds
2024
- Comparison of Computational Predictions for a Cooled High-Pressure Turbine to Data From a Short Duration Experiment
2023
- Effect of Coolant Flowrate on High-Pressure Turbine Tip Flow Structures and Thermal Loading
2023
- Modeling Tip Flow Structures and Heat Transfer in Contemporary Cooled and Uncooled High-Pressure Turbine Blades
2023
- Experimental Determination of Blade Tip Rub Forces in a Multiblade System
Journal of Engineering for Gas Turbines and Power · 2022
- Film Cooling Hole Shape Effects on Turbine Blade Heat Transfer – Part I: Computational Comparison to Experiment
2022
- Journal of Engineering for Gas Turbines and Power×3
- Journal of Turbomachinery×2
- 2018 Joint Propulsion Conference×1
- 52nd AIAA/SAE/ASEE Joint Propulsion Conference×1
- 53rd AIAA/SAE/ASEE Joint Propulsion Conference×1
- Ali Ameri
Engineering · The Ohio State University
- T. I.-P. Shih
Engineering · Purdue University West Lafayette
- William J. Gooding
Engineering · Purdue University West Lafayette
- Guillermo Paniagua
Engineering · Purdue University West Lafayette
- Nicole L. Key
Engineering · Purdue University West Lafayette
This profile was generated automatically from public scholarly data (OpenAlex). Group size and activity levels are estimates derived from co-authorship patterns.
Last updated Jul 19, 2026.
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