Modelling Turbine Acoustic Impedance
We quantify the sensitivity of turbine acoustic impedance to aerodynamic design parameters. Impedance boundary conditions are an influential yet uncertain parameter in predicting the thermoacoustic stability of gas turbine combustors. We extend the semi-actuator disk model to cambered blades, using...
Main Authors: | James Brind, Graham Pullan |
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Format: | Article |
Language: | English |
Published: |
MDPI AG
2021-06-01
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Series: | International Journal of Turbomachinery, Propulsion and Power |
Subjects: | |
Online Access: | https://www.mdpi.com/2504-186X/6/2/18 |
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