Aeroelastic Topology Optimization of a Supersonic Wing, M.Sc. Thesis Sharif University of Technology ; Hadadpour, Hassan (Supervisor) ; Dehghani Firouzabadi, Rouhollah (Supervisor) ; Noorian, Mohammad Ali (Co-Advisor)
Abstract
A series of algorithms developed for performing aeroelastic topology optimization applying stress constraint on a three dimentional structure of a supersonic wing. The structure modeled using finite element method by three dimentional solid hexahedron elements. Bi-directional evolutionary structural optimization method used for developing optimization algorithms. In order to apply supersonic aerodynamic loading and developing aeroelastic model algorithms, the piston aerodynamic theory utilized. In order to apply static pressure loading, the maximum angle of attack of the wing performance is proposed. Using developed MATLAB code by modeling and meshing wing structure in ABAQUS a software...
Cataloging briefAeroelastic Topology Optimization of a Supersonic Wing, M.Sc. Thesis Sharif University of Technology ; Hadadpour, Hassan (Supervisor) ; Dehghani Firouzabadi, Rouhollah (Supervisor) ; Noorian, Mohammad Ali (Co-Advisor)
Abstract
A series of algorithms developed for performing aeroelastic topology optimization applying stress constraint on a three dimentional structure of a supersonic wing. The structure modeled using finite element method by three dimentional solid hexahedron elements. Bi-directional evolutionary structural optimization method used for developing optimization algorithms. In order to apply supersonic aerodynamic loading and developing aeroelastic model algorithms, the piston aerodynamic theory utilized. In order to apply static pressure loading, the maximum angle of attack of the wing performance is proposed. Using developed MATLAB code by modeling and meshing wing structure in ABAQUS a software...
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