Supersonic wind tunnel tests on a 1/12th scale model of the bristol type 188 research aircraft part 1 M = 1.4 to 2.0 part 2 M = 2.0 to 2.7

dc.contributor.author	C. R. Taylor	en_US
dc.contributor.author	T. A. Cook	en_US
dc.date.accessioned	2014-10-20T11:04:19Z
dc.date.available	2014-10-20T11:04:19Z
dc.date.issued	1965	en_US
dc.identifier.other	ARC/CP-818	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/831
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Supersonic wind tunnel tests on a 1/12th scale model of the bristol type 188 research aircraft part 1 M = 1.4 to 2.0 part 2 M = 2.0 to 2.7	en_US