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
更好的逼近涡轮发机，应用成熟的非均匀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.
摘要为了使气更好的逼近涡轮发机，应用成熟的非均匀B样条来拟合部件特性。
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