Sensitivity Analysis for the Control of Oblique Shock Wave/laminar Boundary Layer Interactions at Mach 5.92 (AIAA 2017-4312)
Fluid dynamics (Conference)
2017-01-01
14 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Interaction of an Oblique Shock with a Transitional Mach 5.92 Boundary Layer (AIAA 2016-3647)
British Library Conference Proceedings | 2016
|British Library Conference Proceedings | 2018
|Frequency Analysis of Oblique Shock Wave Boundary Layer Interaction (AIAA 2017-0988)
British Library Conference Proceedings | 2017
|