Shock-Boundary Layer Interaction due to a Sharp Unswept Fin in a Mach 2 Flow (AIAA 2015-1517)
Aerospace sciences meeting
2015-01-01
12 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Investigation of Unswept Normal Shock Wave-Turbulent-Boundary-Layer Interaction Control
Online Contents | 2009
|British Library Conference Proceedings | 2014
|