Wind tunnel tests at mach numbers up to 1.8 on a model with .03 scale wings and nacelles of a twin-engined supersonic aircraft (Bristol 188)

dc.contributor.author	E.P. Sutton	en_US
dc.contributor.author	P.G. Hutton	en_US
dc.contributor.author	L.C. Squire	en_US
dc.date.accessioned	2014-10-20T11:03:58Z
dc.date.available	2014-10-20T11:03:58Z
dc.date.issued	1965	en_US
dc.identifier.other	ARC/CP-798	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/811
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Wind tunnel tests at mach numbers up to 1.8 on a model with .03 scale wings and nacelles of a twin-engined supersonic aircraft (Bristol 188)	en_US