An artificial neural network approach for aerodynamic performance retention in airframe noise reduction design of a 3D swept wing model
noise reduction、aerodynamic performance、artificial neural network、airframe noise、neural network approach、numerical results、back propagation、acoustic analogy、training sample、civil aircraft、hybrid method、BP network、high lift
29
TP3;O24
The work was supported by the National Basic Research Pro-gram of China 2014CB744800
2016-11-10(万方平台首次上网日期,不代表论文的发表时间)
共13页
1213-1225