Numerical Analysis on Transient Response of Turbine Blandes by Partial Admission

부분 유입되는 터빈 블레이드의 과도 응답 특성에 대한 수치 해석

  • 이진갑 (경희대학교 기계공학과)
  • Published : 1998.05.01

Abstract

A numerical analysis is presented for the transient behavior of a rotating turbines blades. The response due to partial admission during start-up and resonance pass is considered, Modal analysis and numerical integation method are used for solving the problems A theory for determining the material and aerodynamic damping values of turbine blades is presented. The damping values of the various modeling of blaes-uniform beam and tapered twisted beam-are calculated and the influence on blades response is investigated. The effect of angular velocity on transient response are also shown.

Keywords

References

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