Non-uniform rational B-splines (NURBS) was used to fit component characteristics of aerothermodynamic model for approaching turbine engine.
摘要为了使气动热力模型
逼近涡轮发动机，应用
熟非均匀B样条来拟合
件特性。
Non-uniform rational B-splines (NURBS) was used to fit component characteristics of aerothermodynamic model for approaching turbine engine.
摘要为了使气动热力模型逼近涡轮发动机，应用熟非均匀B样条来拟合件特性。
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