Skip to main navigation Skip to search Skip to main content

Aerodynamic design system & ideology of air-cooled turbine and its application to gas turbines

Research output: Contribution to journalArticlepeer-review

Abstract

This study introduces the development of an aerodynamic design system and ideology for air-cooled turbines in advanced gas turbines. There are three parts in all. The development of an aerodynamic design system for air-cooled turbines and the hierarchical optimization process are introduced in the first part. The measures to improve the stability and accuracy of aerodynamic calculations are introduced in the second part. Finally, the aerodynamic design ideology of air-cooled turbines is introduced in the third part.

Original languageEnglish
Pages (from-to)1841-1848
Number of pages8
JournalKung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics
Volume30
Issue number11
StatePublished - Nov 2009

Keywords

  • Aerodynamic design system
  • Air-cooled turbine
  • Design ideology

Fingerprint

Dive into the research topics of 'Aerodynamic design system & ideology of air-cooled turbine and its application to gas turbines'. Together they form a unique fingerprint.

Cite this