01 - Aircraft Design and Integrated Systems
AN ADJOINT-BASDF AERO-STRUCTURAL DESIGN OPTIMIZATION METHOD USING DYNAMIC MESH TECHNOLOGY
J. Guo¹, Y. Li, School of Aeronautics, Northwestern Polytechnical University, China; M. Xu¹; ¹School of Astronautics, Northwestern Polytechnical University, China
In this paper an aero-structural design optimization method is built based on the adjoint approach [1] and the open CFD code (SU2). In this methodology, dynamic mesh technology is used to construct the new aerodynamic grid in each step of optimization.