Exploratory tests on a thin delta wing in the flow field of a rectangular foreplane at mach number 1.8

dc.contributor.author	M. S. Igglesden	en_US
dc.contributor.author	L. J. Beecham	en_US
dc.date.accessioned	2014-10-20T11:02:41Z
dc.date.available	2014-10-20T11:02:41Z
dc.date.issued	1961	en_US
dc.identifier.other	ARC/CP-530	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/543
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Exploratory tests on a thin delta wing in the flow field of a rectangular foreplane at mach number 1.8	en_US