There was a large discrepancy between the results obtained by energy balance method and by aerodynamicmethod.
空气动力学方法的结果与能量平衡法有较大差异。
2
In this dissertation, Numerical Aerodynamic Optimization method is attempted to apply in the inlet design.
本文尝试采用气动优化设计方法进行进气道的设计。
3
An aerodynamic optimization method is described which is based on dynamic boundary control. This method is according to the idea of controlling the boundary of transforming object.