A Sequential Linear Programming technique, known as the method of centers, is the driver of an aerodynamic shape optimization framework on unstructured meshes. The first order information required by this technique, functional values and their gradients, are computed by a median-dual flow/adjoint solver which is coupled to an analytical shape parameterization. Functional and geometric constraints are easily handled by the algorithm which appears to be very effective in obtaining efficiently near-optimal designs. Shape optimization results are presented for transonic as well as supersonic flows involving appreciable shape deformations.

Aerodynamic shape optimization, Sequential Linear Programming, Unstructured meshes, Adjoint equations"
Acceleration of convergence (msc 65Bxx), Optimization and variational techniques (msc 65K10), Inverse problems (msc 65N21), Compressible fluids and gas dynamics, general (msc 76Nxx)
Life Sciences (theme 5), Energy (theme 4)
CWI
Modelling, Analysis and Simulation [MAS]
Scientific Computing

Carpentieri, G, van Tooren, M.J.L, & Koren, B. (2007). Aerodynamic shape optimization by means of sequential linear programming techniques. Modelling, Analysis and Simulation [MAS]. CWI.