Transpiration Cooled Turbines-Reference-Cited by-同舟云学术

Transpiration Cooled Turbines

Published:1970-06 Issue:1 Volume:185 Page:943-951
ISSN:0020-3483
Container-title:Proceedings of the Institution of Mechanical Engineers
language:en
Short-container-title:Proceedings of the Institution of Mechanical Engineers

Author:

Bayley F. J.¹,Turner A. B.²

Affiliation:

1. Professor of Mechanical Engineering, School of Applied Sciences, University of Sussex, Brighton

2. Mechanical Engineering Laboratories, School of Applied Sciences, University of Sussex, Brighton

Abstract

This paper lists the steps in the development chain of air cooling for gas turbine components, and represents transpiration cooling as the ultimate method. The three modes of heat transfer involved in transpiration cooling, gas side heat transfer, coolant side heat transfer and interstitial heat transfer, are discussed separately. Finally, consideration is given to the practical problems of transpiration cooling in advanced gas turbines.

Publisher

SAGE Publications

Subject

General Engineering

Link

http://journals.sagepub.com/doi/pdf/10.1243/PIME_PROC_1970_185_107_02

Reference8 articles.

1. Calculation of boundary-layer development using the turbulent energy equation

2. Local Heat Transfer Measurements on a Gas Turbine Blade

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