We present a reduced-order modelling technique for analyzing the unsteady subsonic aerodynamic flow about isolated airfoils. To start, we model the flow using the time-linearized full potential equation. The linearized potential equation is discretized on a computational mesh composed of quadrilater
Airfoil cascade in unsteady eddy flow
β Scribed by V. A. Yudin
- Publisher
- SP MAIK Nauka/Interperiodica
- Year
- 1994
- Tongue
- English
- Weight
- 315 KB
- Volume
- 35
- Category
- Article
- ISSN
- 0021-8944
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