Hybrid LES Approach for Practical Turbomachinery Flows-Part II: Further Applications (2012)
Attributed to:
CAMBRIDGE UGTP WHOLE ENGINE COMPUTATIONAL AEROACOUSTICS CONSORTIUM
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Digital Object Identifier: http://dx.doi.org/10.1115/1.4003062
Publication URI: http://dx.doi.org/10.1115/1.4003062
Type: Journal Article/Review
Parent Publication: Journal of Turbomachinery
Issue: 2
ISSN: 0889-504X