未來展望

本程式對於空化初始已模擬成功，唯對於基本現象仍有些許的誤差，正 是未來需要再加以改進的地方，首先將網格點做一較完整的規劃如下：

圖 5.1 （上）本文之計算網格，（下）加密後之計算網格

圖 5.1（下）為在翼形的上表面等間距分佈 200 等分，並在 J 方向 0.1c 上將 格點集中，再均勻的散出去，為的是在 suction side 壓力降的地方能計算準

確，但是網格加密後，數值方法也必須加以改進，否則在流場參數的計算上 會有震盪的情形出現。

接著，二維翼形的計算發展完成之後，將進一步轉到三維翼形上面，

畢竟在實務上三維仍是主要的發展趨勢，利用在二維翼計算上得到的經驗和 心得，希望在三維翼形能有滿意的結果。

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在文檔中 基因演算法於二維空蝕水翼逆向設計及最佳設計之應用(3/3) (頁 69-75)