Computation of unsteady turbomachinery flows: Part 2-LES and hybrids (2011)
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/10.1016/j.paerosci.2011.07.002
Publication URI: http://dx.doi.org/10.1016/j.paerosci.2011.07.002
Type: Journal Article/Review
Parent Publication: Progress in Aerospace Sciences
Issue: 7