Efficient prediction of classical flutter stability of turbomachinery blade using the boundary element type numerical method (Q2301635)
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| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Efficient prediction of classical flutter stability of turbomachinery blade using the boundary element type numerical method |
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Efficient prediction of classical flutter stability of turbomachinery blade using the boundary element type numerical method (English)
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25 February 2020
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turbomachinery
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aeroelasticity
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panel method (PM)
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aerodynamic damping (AD)
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traveling wave mode (TWM)
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classical flutter
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boundary element method (BEM)
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