Hypersonic boundary-layer disturbances on a cooled, slender cone at Mach 6
LA Paquin, SN Skinner, SJ Laurence - Journal of Spacecraft and …, 2023 - arc.aiaa.org
This paper presents an experimental study of the effect of wall cooling on the boundary-layer
structures of a sharp-nosed, 5° half-angle cone in Mach 6 flow. An experimental …
structures of a sharp-nosed, 5° half-angle cone in Mach 6 flow. An experimental …
Effect of cooling on hypersonic Boundary-Layer stability
L Paquin - 2022 - search.proquest.com
The prediction of boundary-layer transition on hypersonic vehicles has long been
considered a primary design concern due to extreme levels of heating and dynamic …
considered a primary design concern due to extreme levels of heating and dynamic …