Non-uniform rational B-splines (NURBS) was used to fit component characteristics of aerothermodynamic model for approaching turbine engine.
摘要为了使气动热
模型更好
逼近涡轮发动机，应用成熟
均
B
来拟合部件特性。
一致有理B
(一种用数学描绘曲线和不规则形状
方法)
均
有理BNon-uniform rational B-splines (NURBS) was used to fit component characteristics of aerothermodynamic model for approaching turbine engine.
摘要为了使气动热模型更好逼近涡轮发动机，应用成熟均B来拟合部件特性。
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