Measurements of the effect of surface cooling on boundary layer transition on a 15 degrees cone part 2 tests at M = 3 and M = 4 in the 5 in. x 5 in. no. 5 wind tunnel at R.A.E. Farnborough

dc.contributor.author	J. G. Woodley	en_US
dc.date.accessioned	2014-10-20T11:02:32Z
dc.date.available	2014-10-20T11:02:32Z
dc.date.issued	1960	en_US
dc.identifier.other	ARC/CP-479	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/492
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 2 tests at M = 3 and M = 4 in the 5 in. x 5 in. no. 5 wind tunnel at R.A.E. Farnborough	en_US