Preliminary Design Analysis of an Axial-Flow Turbine

축류터어빈의 기초설계 해석

  • 구삼옥 (한국기계연구원 창원본소 항공기계실) ;
  • 최동환 (한국기계연구원 창원본소 항공기계실)
  • Published : 1985.06.29

Abstract

A review on the design analysis of an axial-flow turbine is presented. Followed by a brief introduction to the fundamentals on an axial-flow turbine, a design procedure is described with a sample design of one for a small turbo-jet engine. Design procedure is composed of two parts: one-dimensional analysis of three-dimensional effects based on radial equilibrium theory. The method described herein is so simple and rapid that it can be applied to the preliminary design analysis of turbo-machinery equipped with axial-flow turbines.

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