Transitional Shock-Wave/Boundary-Layer Interactions in Intakes at Incidence
Advances in simulation of wing and nacelle stall: results of the closing symposium of the DFG Research Unit FOR 1066 ; 2014 ; Braunschweig, Germany
2016-01-01
14 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Shock Wave-Boundary-Layer Interactions in Subsonic Intakes at High Incidence (AIAA 2015-0067)
British Library Conference Proceedings | 2015
|British Library Conference Proceedings | 2018
|