Performance of the 36 x 35 in. slotted transonic working section of the R.A.E. bedford 3-ft wind tunnel

dc.contributor.author	E. P. Sutton	en_US
dc.contributor.author	M. T. Caiger	en_US
dc.contributor.author	A. Stanbrook	en_US
dc.date.accessioned	2014-10-21T15:55:28Z
dc.date.available	2014-10-21T15:55:28Z
dc.date.issued	1960	en_US
dc.identifier.other	ARC/R&M-3228	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3801
dc.description.abstract	A 36 x 35 in. transonic working section with slotted walls on all four sides is described. It is interchangeable with the original supersonic working section of the 3-ft. tunnel, and is used for tests at Mach numbers up to 1.25. The performance of the working section is summarised, with particular attention to effects of varying the angles of inclination of the upper and lower walls to the tunnel axis.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Performance of the 36 x 35 in. slotted transonic working section of the R.A.E. bedford 3-ft wind tunnel	en_US