Non-uniform rational B-splines (NURBS) was used to fit component characteristics of aerothermodynamic model for approaching turbine engine.

 
  • 摘要為了使氣動(dòng)熱力模型更好的逼近渦輪發(fā)動(dòng)機,應用成熟的非均勻B樣條來(lái)擬合部件特性。
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