There was a large discrepancy between the results obtained by energy balance method and by aerodynamic method.
空气动力学方法的结果与能量平衡法有较大差异。
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。
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.
本文根据控制变形物体边界变化的思想，建立了一种基于动态边界控制的气动优化设计方法。
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