Rotating Instabilities in Shrouded Low Pressure Turbine at Design and Off-Design Conditions
Author:
Affiliation:
1. University of Toulouse, ISAE-SUPAERO Department of Aerodynamics, Energetics and Propulsion, , Toulouse 31400 , France
2. Safran Aircraft Engines Design Office, Low Pressure Turbine Aerodynamic, , Moissy-Cramayel 77550 , France
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
https://asmedigitalcollection.asme.org/turbomachinery/article-pdf/145/11/111006/7048059/turbo_145_11_111006.pdf
Reference30 articles.
1. Loss Mechanisms in Turbomachines;Denton;ASME J. Turbomach.,1993
2. Quantifying Loss Mechanisms in Turbine Tip Shroud Cavity Flows;Palmer;ASME J. Turbomach.,2016
3. Making Use of Labyrinth Interaction Flow;Pfau;ASME J. Turbomach.,2007
4. Numerical Investigation of the Interaction Between Mainstream and Tip Shroud Leakage Flow in a 2-Stage Low Pressure Turbine;Jia;J. Thermal Sci.,2014
5. Unsteady Flow Interactions Within the Inlet Cavity of a Turbine Rotor Tip Labyrinth Seal;Pfau,2003
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