Prediction of flutter effects on transient flow structure and aeroelasticity of low-pressure turbine cascade using direct numerical simulations

Author:

Win Naung Shine,Nakhchi Mahdi ErfanianORCID,Rahmati MohammadORCID

Funder

Engineering and Physical Sciences Research Council

Publisher

Elsevier BV

Reference44 articles.

1. Design of high accuracy cylindrical profile measurement model for low-pressure turbine shaft of aero engine;Sun;Aerosp. Sci. Technol.,2019

2. Ultra-High Lift Blades for Low Pressure Turbines;Himmel,2010

3. Bladerow interactions, transition, and high-lift aerofoils in low-pressure turbines;Hodson;Annu. Rev. Fluid Mech.,2005

4. Unsteady boundary-layer transition in low-pressure turbines;Coull;J. Fluid Mech.,2011

5. A design method to prevent low pressure turbine blade flutter;Panovsky;J. Eng. Gas Turbines Power,1999

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