From: Computational Aerodynamics: Solvers and Shape Optimization Date of download: 11/7/2017 Copyright © ASME. All rights reserved. From: Computational Aerodynamics: Solvers and Shape Optimization J. Heat Transfer. 2012;135(1):011002-011002-9. doi:10.1115/1.4007649 Figure Legend: Computed velocity profiles for 2D laminar boundary layer—finite volume cell-centered formulation with a CUSP dissipation. Similarity solution of both components of the velocity is verified.

From: Computational Aerodynamics: Solvers and Shape Optimization Date of download: 11/7/2017 Copyright © ASME. All rights reserved. From: Computational Aerodynamics: Solvers and Shape Optimization J. Heat Transfer. 2012;135(1):011002-011002-9. doi:10.1115/1.4007649 Figure Legend: Business jet configuration. Iso-CP Navier–Stokes solution with 240 blocks and 5.8 million mesh points. M = 0.82, α = 1.0 deg.

From: Computational Aerodynamics: Solvers and Shape Optimization Date of download: 11/7/2017 Copyright © ASME. All rights reserved. From: Computational Aerodynamics: Solvers and Shape Optimization J. Heat Transfer. 2012;135(1):011002-011002-9. doi:10.1115/1.4007649 Figure Legend: Density contours on the surface of business jet: left original configuration—right optimized