TY - JOUR
T1 - An Embedded Ghost-Fluid Method for Compressible Flow in Complex Geometry
AU - Al-Marouf, Mohamad
AU - Samtaney, Ravi
N1 - KAUST Repository Item: Exported on 2020-10-01
Acknowledged KAUST grant number(s): URF/1/1394-01
Acknowledgements: URF/1/1394-01, KAUST
PY - 2016/4
Y1 - 2016/4
N2 - We present an embedded ghost-fluid method for numerical solutions of the compressible Navier Stokes (CNS) equations in arbitrary complex domains. The PDE multidimensional extrapolation approach of Aslam [1] is used to reconstruct the solution in the ghost-fluid regions and impose boundary conditions at the fluid-solid interface. The CNS equations are numerically solved by the second order multidimensional upwind method of Colella [2] and Saltzman [3]. Block-structured adaptive mesh refinement implemented under the Chombo framework is utilized to reduce the computational cost while keeping high-resolution mesh around the embedded boundary and regions of high gradient solutions. Numerical examples with different Reynolds numbers for low and high Mach number flow will be presented. We compare our simulation results with other reported experimental and computational results. The significance and advantages of our implementation, which revolve around balancing between the solution accuracy and implementation difficulties, are briefly discussed as well. © 2016 Trans Tech Publications.
AB - We present an embedded ghost-fluid method for numerical solutions of the compressible Navier Stokes (CNS) equations in arbitrary complex domains. The PDE multidimensional extrapolation approach of Aslam [1] is used to reconstruct the solution in the ghost-fluid regions and impose boundary conditions at the fluid-solid interface. The CNS equations are numerically solved by the second order multidimensional upwind method of Colella [2] and Saltzman [3]. Block-structured adaptive mesh refinement implemented under the Chombo framework is utilized to reduce the computational cost while keeping high-resolution mesh around the embedded boundary and regions of high gradient solutions. Numerical examples with different Reynolds numbers for low and high Mach number flow will be presented. We compare our simulation results with other reported experimental and computational results. The significance and advantages of our implementation, which revolve around balancing between the solution accuracy and implementation difficulties, are briefly discussed as well. © 2016 Trans Tech Publications.
UR - http://hdl.handle.net/10754/621376
UR - https://www.scientific.net/DDF.366.31
UR - http://www.scopus.com/inward/record.url?scp=84973462046&partnerID=8YFLogxK
U2 - 10.4028/www.scientific.net/DDF.366.31
DO - 10.4028/www.scientific.net/DDF.366.31
M3 - Article
SN - 1662-9507
VL - 366
SP - 31
EP - 39
JO - Defect and Diffusion Forum
JF - Defect and Diffusion Forum
ER -