This article introduces a designing means of mold of the fibre winding solid rocket motor combustion chamber shell.
介绍一种固体火箭发动机燃烧室壳体纤维缠绕芯模的设计。
Filter the redundancy vertex in STL solid is very important. The algorithm is successful to deal with 3d graphic in realistic mold flow simulation software.
而剔除STL面片数据中的冗余顶点是重构的关键，该算法已经成功应用于三维真实感注塑模流动模拟软件的3d图形处理。
The results show that due to the strong jet impingement on the narrow face in mold, solid shell near the impingement point is very thin.
研究表明，钢液对结晶器窄面的冲击严重，导致在冲击点附近的凝固坯壳较薄。
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