Gun tunnel measurements of lift, drag and pitching moment on a 20 degrees cone, a flat delta and a caret delta wing at a mach number of 8.3

dc.contributor.author	T. Opatowski	en_US
dc.date.accessioned	2014-10-20T11:04:48Z
dc.date.available	2014-10-20T11:04:48Z
dc.date.issued	1966	en_US
dc.identifier.other	ARC/CP-908	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/921
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Gun tunnel measurements of lift, drag and pitching moment on a 20 degrees cone, a flat delta and a caret delta wing at a mach number of 8.3	en_US