最后介绍了近无激波机翼修型的工程设计方法。
Finally, an engineering approach for nearly shock-free wing design is introduced.
在曲线修型技术的基础上，进一步对曲面修型技术进行研究。
On the basis of the shape modification of curves, it extends the technique of above to the shape modification of surfaces.
系统总结了权因子的几何意义，及对曲线、曲面的修型原理，并给出了其实现方法。
It systemically summarizes the geometry meanings of weights and the principle of the shape modification of curves and surfaces. This paper gives a method of implementing.
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