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- W844457588 abstract "A finite difference code has been developed and applied to numerical analysis of unsteady separating flows over an oscillating airfoil. The full as well as thin-layer Navier-Stokes equations have been solved with Spalart-Allmaras one-equation turbulence model. The time-marching integration of the governing equations by LU-SGS implicit scheme has been improved by using Matsuno's . Numerical computations for three different unsteady flow conditions, corresponding to attached flows, light dynamic stall and deep dynamic stall, are compared with experimental data. The comparison reveals that the use of the full Navier-Stokes equations do not provide any advantages over that of the thin-layer Navier-Stokes equations when the simple Spalart-Allmaras one-equation turbulence model is used." @default.
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- W844457588 date "1997-01-01" @default.
- W844457588 modified "2023-09-23" @default.
- W844457588 title "Numerical Analysis of Dynamic Stall of NACA0015 Airfoil" @default.
- W844457588 hasPublicationYear "1997" @default.
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