A Method of Map Extrapolation for Unequal and Partial Admission in a Double Entry Turbine
Author:
Affiliation:
1. Department of Mechanical Engineering, Imperial College, London SW7 2BX, UK e-mail:
2. Department of Mechanical Engineering, University of Bath, Bath BA2 7AY, UK e-mail:
3. ABB Turbo Systems, Baden 5401, Switzerland e-mail:
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4025763/6299406/turbo_136_06_061019.pdf
Reference13 articles.
1. Unsteady Performance of a Double Entry Turbocharger Turbine With a Comparison to Steady Flow Conditions;ASME J. Turbomach.,2012
2. Comparison Between Steady and Unsteady Double-Entry Turbine Performance Using the Quasi-Steady Assumption;ASME J. Turbomach.,2011
3. The Effect of Unequal Admission on the Performance and Loss Generation in a Double-Entry Turbocharger Turbine;ASME J. Turbomach.,2012
4. Copeland, C., 2010, “The Evaluation of Steady and Pulsating Flow Performance of a Double-Entry Turbocharger Turbine,” Ph.D. thesis, Imperial College of Science, Technology, and Medicine, University of London, London, UK.
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1. A comparison study of loss generation between twin-entry and double-entry volutes of nozzled mixed-flow turbines;International Journal of Engine Research;2023-09-26
2. Unsteady gasdynamic modeling of double-entry turbine integrated with engine exhaust manifolds;Proceedings of the Institution of Mechanical Engineers, Part D: Journal of Automobile Engineering;2023-09-08
3. An Experimental and Modeling Strategy for Obtaining Complete Characteristic Maps of Dual-Volute Radial Inflow Turbines;Journal of Engineering for Gas Turbines and Power;2021-03-31
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