The goal of this dissertation is to apply Simulated Annealing Algorithm to aerodynamic shape optimization problems on the CFD-Solver and to develop a new gradient free optimization method that could decrease time cost greatly for aerodynamics problems.

• 本文的主要目的是:结合流场的正交分解算法,将模拟退火算法应用于气动外形优化设计领域,致力于发展一种不依赖于梯度信息同时可以极大降低计算开销的新型气动外形优化设计方法。