Investigation of a Cylinder-Induced Transitional Shock Wave-Boundary Layer Interaction using Laser Diagnostics (AIAA 2016-4321)
32nd AIAA aerodynamic measurement technology and ground testing conference 2016 ; 2016 ; Washington D.C
01.01.2016
21 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
British Library Conference Proceedings | 2017
|Panel Flutter Induced by Transitional Shock Wave Boundary Layer Interaction (AIAA 2018-3548)
British Library Conference Proceedings | 2018
|