Some calculations of conditions at the intersection of a weak shock wave with a strong shock

dc.contributor.author	I. McGregor	en_US
dc.date.accessioned	2014-10-21T15:50:50Z
dc.date.available	2014-10-21T15:50:50Z
dc.date.issued	1972	en_US
dc.identifier.other	ARC/R&M-3728	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3005
dc.description.abstract	Some comprehensive calculations of the flow conditions resulting from the intersection of a weak shock wave with a strong shock are presented and discussed, for a range of upstream Mach numbers between 1.4 and 2.8. Such flows are of interest in connection with the sub-critical stability of air intakes, for example, and in the interaction of shock waves and boundary layers.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Some calculations of conditions at the intersection of a weak shock wave with a strong shock	en_US