Numerical simulations of turbulent spots in supersonic boundary layers: Effects of Mach number and wall temperature (2012)
Attributed to:
Supercomputing Resources and Support for the UK Applied Aerodynamics Consortium 2 (2007-2010)
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Digital Object Identifier: http://dx.doi.org/10.1016/j.paerosci.2011.08.002
Publication URI: http://dx.doi.org/10.1016/j.paerosci.2011.08.002
Type: Journal Article/Review
Parent Publication: Progress in Aerospace Sciences