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更好的逼近涡轮发动机，应用成熟的
B样条来拟合部件特性。
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更好的逼近涡轮发动机，应用成熟的B样条来拟合部件特性。
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