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
热力模型更好的逼近涡轮
，应用成熟的非均匀B样条来
合部件特
。
Non-uniform rational B-splines (NURBS) was used to fit component characteristics of aerothermodynamic model for approaching turbine engine.
摘要为了使气热力模型更好的逼近涡轮，应用成熟的非均匀B样条来合部件特。
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