Near-Stall Modelling of a Pitching Airfoil at High Incidence, Mach Number and Reduced Frequency
The prediction accuracy of aeroelastic stability in fans and compressors depends crucially on the accuracy of the underlying aerodynamic predictions. The prevalent approach in the field solves the unsteady Reynolds-averaged Navier—Stokes equations in the presence of blade vibration. Given the unstea...
Main Authors: | , |
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Format: | Article |
Language: | English |
Published: |
MDPI AG
2022-09-01
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Series: | International Journal of Turbomachinery, Propulsion and Power |
Subjects: | |
Online Access: | https://www.mdpi.com/2504-186X/7/4/26 |