1. 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): doi: /
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.

2. 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): doi: /
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.

3. 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): doi: /
Figure Legend:
Density contours on the surface of business jet: left original configuration—right optimized