Understanding Capacity Sensitivity of Cooled Transonic Nozzle Guide Vanes: A Parametric Experimental and Computational Study of the Impact of Trailing Edge Geometry
Author:
Affiliation:
1. Department of Engineer Science, University of Oxford, Oxford OX2 0ES, UK
2. Rolls-Royce plc, WH88, P.O. Box 3, Filton BS34 7QE, UK
3. Department of Engineering Science, University of Oxford, Oxford OX2 0ES, UK
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4050068/6672930/turbo_143_5_051001.pdf
Reference15 articles.
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3. Experimental Measurements of Gas Turbine Flow Capacity Using a Novel Transient Technique;Povey;ASME J. Turbomach.,2011
4. ECAT: An Engine Component Aerothermal Facility at the University of Oxford;Kirollos,2017
5. Analysis of Ultra-Low Uncertainty Gas Turbine Flow Capacity Measurement Techniques;Burdett;Proc. Inst. Mech. Eng. Part A: J. Power Energy.,2020
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1. Experimental Study of Impact of In-Service Deterioration on Aerodynamic Performance of High-Pressure Nozzle Guide Vanes;Journal of Turbomachinery;2023-03-02
2. Lean-Burn Combustor Simulator for an Engine-Component Test Facility: An Experimental and Computational Study;Journal of Turbomachinery;2023-01-30
3. Impact of Trailing Edge Overhang Length on the Loss Characteristics of Fully Cooled Transonic Nozzle Guide Vanes;Journal of Turbomachinery;2022-12-06
4. Experimental Study of Impact of In-Service Deterioration on Thermal Performance of High-Pressure Nozzle Guide Vanes;Journal of Turbomachinery;2022-11-07
5. Annular Dump Diffuser and Deswirl System for Back-Pressure Control in Engine-Scale Transonic Annular Cascade;Journal of Turbomachinery;2022-11-04
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