IMPORTANT NOTICE: EPrints is currently undergoing maintenance and you will be unable to log in from 4PM on Tuesday 17th October, 2017. The maintenance is due to be completed within a week. If you have any questions, please contact eprints@lincoln.ac.uk.

Effect of hole shape on blade cooling effectiveness

Yao, Jun and Sian, Sohan and Khan, J and Yao, Yufeng (2010) Effect of hole shape on blade cooling effectiveness. In: AIAA 48th Aerospace Sciences Meeting, Jan, 2010, Orlando, FL, USA.

Full text not available from this repository.

Item Type:Conference or Workshop contribution (Presentation)
Item Status:Live Archive

Abstract

See paper published

Additional Information:See paper published
Keywords:Hole shpae, cooling, CFD, Effectiveness
Subjects:F Physical Sciences > F343 Computational Physics
H Engineering > H440 Aerodynamics
H Engineering > H321 Turbine Technology
Divisions:College of Science > School of Engineering
ID Code:5445
Deposited On:06 May 2012 23:10

Repository Staff Only: item control page