Abstract
A three-dimensional Euler code is applied to a series of configurations of increasing complexity. Comparisons are made to experiments, or to other computations when the former is not available. The method uses the multigrid approach on sets of equally spaced Cartesian grid cells. A unique and robust implementation of the body surface boundary condition on grid cells not aligned with the surface provides accurate results on relatively coarse grids. All computational results are compared to experimental data with good agreement exhibited over a wide range of flight conditions. The solution accuracy is assessed for the Onera M-6 wing, with errors due to grid resolution of less than 1% being achieved for the lift and pitching moment coefficients.
Sign-in/Register to access full text options 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
