An immersed boundary method for compressible flows using local grid refinement

• Published in: Journal of computational physics 2007-08, Vol.225 (2), p.2098-2117
• Main Authors: de Tullio, M.D., De Palma, P., Iaccarino, G., Pascazio, G., Napolitano, M.
• Format: Article
• Language: English
• Subjects: Computational techniques; Exact sciences and technology; Finite volume method; Mathematical methods in physics; Physics; Preconditioning; RANS equations; Second-order accuracy; Semi-structured grids
• ISSN: 0021-9991; 1090-2716
• DOI: 10.1016/j.jcp.2007.03.008

This paper combines a state-of-the-art method for solving the three-dimensional preconditioned Navier–Stokes equations for compressible flows with an immersed boundary approach, to provide a Cartesian-grid method for computing complex flows over a wide range of the Mach number. Moreover, a flexible local grid refinement technique is employed to achieve high resolution near the immersed body and in other high-flow-gradient regions at a fraction of the cost required by a uniformly fine grid. The method is validated versus well documented steady and unsteady test problems, for a wide range of both Reynolds and Mach numbers. Finally, and most importantly, for the case of the laminar compressible steady flow past an NACA-0012 airfoil, a thorough mesh-refinement study shows that the method is second-order accurate.