Heat transfer for gas turbine internal cooling

High turbine inlet temperature is required for an efficient gas turbine engine. To maximise the turbine temperature, the internal channel of a turbine blade consists of rib-turbulators to enhance the heat transfer of the cooling air. This report focus on the effect of various rib configurations on c...

Full description

Saved in:
Bibliographic Details
Main Author: Ng, Chean Yuan
Other Authors: Chow Wai Tuck
Format: Final Year Project
Language:English
Published: 2018
Subjects:
Online Access:http://hdl.handle.net/10356/74952
Tags: Add Tag
No Tags, Be the first to tag this record!
Institution: Nanyang Technological University
Language: English