Improvements in the Prediction of Steady and Unsteady Transition and Mixing in Low-Pressure Turbines by Means of Machine-Learnt Closures
Author:
Affiliation:
1. University of Florence Department of Industrial Engineering, , Florence , Italy
2. GE Avio , Rivalta di Torino , Italy
3. University of Melbourne Department of Mechanical Engineering, , Parkville VIC 3010 , Australia
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
https://asmedigitalcollection.asme.org/turbomachinery/article-pdf/146/5/051009/7230217/turbo_146_5_051009.pdf
Reference38 articles.
1. Compressible Direct Numerical Simulation of Low Pressure Turbine—Part II: Effect of Inflow Disturbances;Michelassi;ASME J. Turbomach.,2015
2. The Unsteady Development of a Turbulent Wake Through a Downstream Low-Pressure Turbine Blade Passage;Stieger;ASME J. Turbomach.,2005
3. Bladerow Interactions, Transition, and High-Lift Aerofoils in Low-Pressure Turbines;Hodson;Annu. Rev. Fluid Mech.,2005
4. Performance Impacts Due to Wake Mixing in Axial Flow Turbomachinery;Praisner,2006
5. Fluid Dynamics of Axial Turbomachinery: Blade-and Stage-Level Simulations and Models;Sandberg;Annu. Rev. Fluid. Mech.,2022
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