Micro vortex generator control of axisymmetric high-speed laminar boundary layer separation (2014)
Attributed to:
Shock-induced separation of hypersonic transitional boundary layers
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Digital Object Identifier: http://dx.doi.org/10.1007/s00193-014-0514-7
Publication URI: http://dx.doi.org/10.1007/s00193-014-0514-7
Type: Journal Article/Review
Parent Publication: Shock Waves
Issue: 5