Skip to main content

Research Repository

Advanced Search

The effect of hole shape on blade cooling effectiveness

Yao, Yufeng; Yao, Jun

Authors

Yufeng Yao Yufeng.Yao@uwe.ac.uk
Professor in Aerospace Engineering

Dr Jun Yao Jun.Yao@uwe.ac.uk
Senior Lecturer Aerospace Themofluids



Citation

Yao, Y., & Yao, J. (2011). The effect of hole shape on blade cooling effectiveness. International Journal of Engineering Systems Modelling and Simulation, 2(4), 242-248. https://doi.org/10.1504/IJESMS.2010.038144

Journal Article Type Article
Publication Date Jan 1, 2011
Journal International Journal of Engineering Systems Modelling and Simulations
Print ISSN 1755-9758
Publisher Inderscience
Peer Reviewed Not Peer Reviewed
Volume 2
Issue 4
Pages 242-248
DOI https://doi.org/10.1504/IJESMS.2010.038144
Keywords blade cooling effectiveness, hole shape, computational fluid dynamics, CFD, high temperature, turbine blades, service lifetime, cooling hole geometries, simulation, modelling, penetration depth, coolant jet flow, entrainment, hot fluids, vortex structures
Public URL https://uwe-repository.worktribe.com/output/972500
Publisher URL http://dx.doi.org/10.1504/IJESMS.2010.038144