Development of an unstructured mesh/Navier-Stokes method for aerodynamics of aircraft with ice accretions
| Autor: | Steven C. Caruso |
|---|---|
| Rok vydání: | 1990 |
| Předmět: |
Airfoil
Leading edge Finite volume method business.industry Aerodynamics Computational fluid dynamics Computational physics Physics::Fluid Dynamics Mesh generation Triangle mesh Astrophysics::Earth and Planetary Astrophysics Aerospace engineering business Physics::Atmospheric and Oceanic Physics Icing Mathematics |
| Zdroj: | 28th Aerospace Sciences Meeting. |
| DOI: | 10.2514/6.1990-758 |
| Popis: | An advanced flowfield prediction method for airfoils with leading edge ice accretions was developed and applied. The method is intended to be eventually used in an aircraft icing analysis. The flowfield is obtained by solving the Euler or Navier-Stokes equations on an unstructured triangular mesh. A new method has been developed to permit efficient mesh generation while providing high grid resolution near complicated airfoil ice accumulations. Unstructured-mesh Euler calculations are presented for clean and iced airfoils; the results are compared to similar structured-mesh calculations to demonstrate the new method's accuracy and efficiency. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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