✦ LIBER ✦

Computational study of unsteady turbulent flows around oscillating and ramping aerofoils

✍ Scribed by G. N. Barakos; D. Drikakis

Publisher: John Wiley and Sons
Year: 2003
Tongue: English
Weight: 890 KB
Volume: 42
Category: Article
ISSN: 0271-2091
DOI: 10.1002/fld.478

No coin nor oath required. For personal study only.

📜 SIMILAR VOLUMES

Simulation of unsteady turbulent flows a

Simulation of unsteady turbulent flows around moving aerofoils using the pseudo-time method

✍ K. J. Badcock; F. Cantariti; I. Hawkins; M. Woodgate; L. Dubuc; B. E. Richards 📂 Article 📅 2000 🏛 John Wiley and Sons 🌐 English ⚖ 275 KB 👁 2 views

The pseudo-time formulation of Jameson has facilitated the use of numerical methods for unsteady flows, these methods have proved successful for steady flows. The formulation uses iterations through pseudo-time to arrive at the next real time approximation. This iteration can be used in a straightfo

Modelling of turbulent transonic flow ar

Modelling of turbulent transonic flow around aerofoils and wings

✍ Müller, Bernhard ;Rizzi, Arthur 📂 Article 📅 1990 🏛 Wiley (John Wiley & Sons) 🌐 English ⚖ 541 KB

Turbulent flows around aerofoils and wings are simulated by solving the two-and three-dimensional Navier-Stokes equations in quadrilaterals and hexahedrons, respectively. Turbulent flow is described by an algebraic eddy viscosity model. Boundary-conforming 0-and 0-0-type meshes are generated by the

Application of local DFD method to simul

Application of local DFD method to simulate unsteady flows around an oscillating circular cylinder

✍ Y. L. Wu; C. Shu 📂 Article 📅 2008 🏛 John Wiley and Sons 🌐 English ⚖ 468 KB

## Abstract In this paper, the recently proposed local domain‐free discretization (DFD) method is applied to simulate incompressible flows around an oscillating circular cylinder. It is found that it is very easy for the local DFD method to handle such moving boundary flow problems. This is because

Computation of the turbulent flow field

Computation of the turbulent flow field around an aerofoil by k-ϵ-γ model in a non-staggered, C-type single-grid system

✍ Kim, Ki Sup ;Chung, Myung Kyoon 📂 Article 📅 1995 🏛 John Wiley and Sons 🌐 English ⚖ 804 KB

The whole turbulent flow field around a two-dimensional aerofoil is solved with a consistent numerical method on a single-grid system and with an intermittency implemented two-equation model, namely the k -c -y turbulence model in elliptic form. In order to solve the numerical instability problem ar