Tests at a mach number of 2.0 on a rectangular, twin-duct air intake with variable geometry, situated in the flow field of a slender wing

dc.contributor.author	M. D. Dobson	en_US
dc.date.accessioned	2014-10-20T11:05:40Z
dc.date.available	2014-10-20T11:05:40Z
dc.date.issued	1970	en_US
dc.identifier.other	ARC/CP-1122	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/1135
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Tests at a mach number of 2.0 on a rectangular, twin-duct air intake with variable geometry, situated in the flow field of a slender wing	en_US