Measurements of the effect of surface cooling on boundary layer transition on a 15 degrees cone part 1 tests at M = 2 and 3 in an 8 in. x 9 in. wind tunnel at R.A.E./Bedford

dc.contributor.author	A. C. Browning	en_US
dc.contributor.author	J. F. W. Crane	en_US
dc.contributor.author	R. J. Monaghan	en_US
dc.date.accessioned	2014-10-20T11:01:47Z
dc.date.available	2014-10-20T11:01:47Z
dc.date.issued	1958	en_US
dc.identifier.other	ARC/CP-381	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/394
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Measurements of the effect of surface cooling on boundary layer transition on a 15 degrees cone part 1 tests at M = 2 and 3 in an 8 in. x 9 in. wind tunnel at R.A.E./Bedford	en_US