A parallel aerostructural shape optimization platform for airplane wings

2019-05-17
Oktay, Erdal
Arpacı, Anıl
Şehitoğlu, Onur Tolga
Akay, Hasan Umur
A parallel design platform is developed for aerostructural shape optimization of airplane wings. The developed tools consist of a panel method-based aerodynamic solver, a finite element-based structural solver, geometry and mesh generation modules and a parallel genetic algorithm optimizer, with emphasis given to automation and fast solutions
Citation Formats
E. Oktay, A. Arpacı, O. T. Şehitoğlu, and H. U. Akay, “A parallel aerostructural shape optimization platform for airplane wings,” Antalya, Turkey, 2019, p. 1, Accessed: 00, 2021. [Online]. Available: https://hdl.handle.net/11511/87785.