Numerical analysis of blade tip leakage flow and shroud heat transfer in gas turbine engines

One of the most critical components of gas turbine engines, rotor blade tip and casing, is exposed to high thermal load. It is a significant challenge to the designer to protect the turbine material from this severe situation. Leakage flow over the blade tip is also one of the important issues to im...

Full description

Bibliographic Details
Main Author: Rahman, Md. Hamidur
Format: Others
Published: 2008
Online Access:http://spectrum.library.concordia.ca/976268/1/MR63240.pdf
Rahman, Md. Hamidur <http://spectrum.library.concordia.ca/view/creators/Rahman=3AMd=2E_Hamidur=3A=3A.html> (2008) Numerical analysis of blade tip leakage flow and shroud heat transfer in gas turbine engines. Masters thesis, Concordia University.