Abstract
This paper presents a two-level strategy for the parallelization of a genetic algorithm coupled to a compressible flow solver designed on unstructured meshes. The resulting algorithm is used for the optimum shape design of aerodynamic configurations. Preliminary results are presented for the optimization of two-dimensional airfoils.
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.
