Effect of Upstream Disturbance on the Development of a Wall-Bounded Plane Jet at Subsonic Mach Numbers with Separated Flow (AIAA 2018-3541)
Fluid dynamics (Conference)
2018-01-01
12 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
AIAA-2019-3541: Aerodynamic Response to a Compliant Panel in Mach 4 Flow
British Library Conference Proceedings | 2019
|British Library Conference Proceedings | 2018
|DataCite | 1913
Electro-optical voltage transformer [3541-34]
British Library Conference Proceedings | 1998
|