Experimental characterisation of the coolant film generated by various gas turbine combustor liner geometrics

In modern, low emission, gas turbine combustion systems the amount of air available for cooling of the flame tube liner is limited. This has led to the development of more complex cooling systems such as cooling tiles i.e. a double skin system, as opposed to the use of more conventional cooling slot...

Full description

Bibliographic Details

Main Author:	Khim Heng Chua
Format:	Default Thesis
Published:	2005
Subjects:	Other engineering not elsewhere classified Film cooling Effusion patch Adiabatic film cooling effectiveness Double skin cooling system Gas turbine combustor liner Cooling film unsteadiness Length scale Mainstream turbulence intensity Engineering not elsewhere classified
Online Access:	https://hdl.handle.net/2134/12704
Tags:	Add Tag No Tags, Be the first to tag this record!