Heat Transfer in Film-Cooled Turbine Blades
Author Information:	Garg, Vijay
Abstract:	The objectives of the study include: (1) Developing tools and models to accurately predict hot gas side heat transfer to a film-cooled turbine blade; (2) Minimizing the injected mass flow for a given cooling efficiency; and (3) Decreasing aerodynamic losses induced by the jet-secondary flow interaction.
Full Text:	PDF
Publication Date:	Aug. 1997
Document ID (CASI):	19980013185
Security Classif.:	Unclassified
Restriction on Access:	Unlimited
Authorized Users:	Publicly available
Copyright Indicator:	No Copyright
Description:	24p
Source Publication:	1996 Coolant Flow Management Workshop/ 157-180; NASA-CP-10195/ (SEE 19980013176)
Available From:	CASI
Format and Price Code:	Hardcopy - Price Code: A03