Interactions between normal shock waves and turbulent boundary layers

dc.contributor.author	G. E. Gadd	en_US
dc.date.accessioned	2014-10-21T15:55:36Z
dc.date.available	2014-10-21T15:55:36Z
dc.date.issued	1961	en_US
dc.identifier.other	ARC/R&M-3262	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3837
dc.description.abstract	A theory, involving a simple new method for turbulent boundary layers, is presented for interactions between normal shocks and turbulent boundary layers on flat surfaces. Experiments in a pipe confirm the theory's general validity. Effects on separation of convex surface curvature and sweepback of the shock are then considered.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Interactions between normal shock waves and turbulent boundary layers	en_US