Numerical Biobjective Optimal Design of Airfoil and Wing
Z. Q. Zhu, Rixin Yu, H. Y. Fu, Y. C. Chen · Journal of Aircraft · 2003
Biobjective and bidisciplinary optimal design of high-performance airfoil and wing applying two kinds of optimization methods and genetic algorithm are discussed. An objective function combination method (OFCM) of constructing a resultant objective function in DOM or a fitness function in GA for biobjective optimization.