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
模型更好的逼近涡轮发动机，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.
摘要为了使气动热模型更好的逼近涡轮发动机，应用成熟的非均匀B样条来拟合部件特性。
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审核，其表达内容亦不代表本软件的观点；若发现问题，欢迎向我们指正。
