Optimization and design of an aircraft”s morphing wing-tip demonstrator for drag reduction at low speed, Part Ⅰ–Aerodynamic optimization using genetic, bee colony and gradient descent algorithms
drag reduction、optimization problem、Monte Carlo method、experimental test、wind tunnel test、gradient method、global optimum
30
U66;TV1
2017-04-12(万方平台首次上网日期,不代表论文的发表时间)
共15页
149-163