TY - GEN
T1 - Immersed boundary method for viscous flow around moving bodies
AU - Yong, Cho
AU - Boluriaan, Said
AU - Morris, Philip J.
N1 - Copyright:
Copyright 2011 Elsevier B.V., All rights reserved.
PY - 2006
Y1 - 2006
N2 - This paper describes a methodology for the simulation of high Reynolds number flow over rigid and moving bodies. The calculations are performed on a structured Cartesian grid regardless of the geometric complexity or motion of the body. The approach is based on a modified version of the Brinkman Penalization method. The spatial derivatives of fluxes are discretized using a Weighted Essentially Non-Oscillatory (WENO) scheme. This paper describes a simple modified penalization method. For high Reynolds number viscous flows, a k-ω turbulence model is implemented. The methodology and its numerical implementation are described. Some simple flow examples are given to assess the accuracy of the technique. Results are then presented for high Reynolds number flow over a fixed and an oscillating airfoil and comparisons are made with experiment. Finally, a three-dimensional implementation of the method is demonstrated.
AB - This paper describes a methodology for the simulation of high Reynolds number flow over rigid and moving bodies. The calculations are performed on a structured Cartesian grid regardless of the geometric complexity or motion of the body. The approach is based on a modified version of the Brinkman Penalization method. The spatial derivatives of fluxes are discretized using a Weighted Essentially Non-Oscillatory (WENO) scheme. This paper describes a simple modified penalization method. For high Reynolds number viscous flows, a k-ω turbulence model is implemented. The methodology and its numerical implementation are described. Some simple flow examples are given to assess the accuracy of the technique. Results are then presented for high Reynolds number flow over a fixed and an oscillating airfoil and comparisons are made with experiment. Finally, a three-dimensional implementation of the method is demonstrated.
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M3 - Conference contribution
AN - SCOPUS:34250883881
SN - 1563478072
SN - 9781563478079
T3 - Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting
SP - 13169
EP - 13180
BT - Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting
T2 - 44th AIAA Aerospace Sciences Meeting 2006
Y2 - 9 January 2006 through 12 January 2006
ER -