A New Experimental Facility to Investigate Combustor–Turbine Interactions in Gas Turbines With Multiple Can Combustors
Author:
Affiliation:
1. Department of Engineering Science, Osney Thermofluids Laboratory, University of Oxford, Osney Mead, Oxford OX2 0ES, UK e-mail:
2. Mitsubishi Heavy Industries, Takasago Research & Development Center, Takasago, Hyogo 676-8686, Japan e-mail:
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Link
http://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/doi/10.1115/1.4028714/6165564/gtp_137_05_051503.pdf
Reference31 articles.
1. Limitations on Gas Turbine Performance Imposed by Large Turbine Cooling Flows;ASME J. Turbomach.,2001
2. Dynamics and Stability of Lean-Premixed Swirl-Stabilized Combustion;Prog. Energy Combust. Sci.,2009
3. Effects of Inlet Temperature Gradients on Turbomachinery Performance;ASME J. Eng. Power,1975
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