The 9 x 3 in. induced-flow high-speed wind tunnel at the national physical laboratory

dc.contributor.author	D. W. Holder	en_US
dc.contributor.author	R. J. North	en_US
dc.date.accessioned	2014-10-21T15:52:49Z
dc.date.available	2014-10-21T15:52:49Z
dc.date.issued	1949	en_US
dc.identifier.other	ARC/R&M-2781	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3332
dc.description.abstract	A 9 X 3 in. high-speed wind tunnel driven by a compressed-air injector has been built in the Aerodynamics Division of the National Physical Laboratory. The tunnel operates at roughly atmospheric stagnation pressure and has so far been used to give Mach numbers up to 1.8. The general arrangement of the tunnel and the preliminary calibration, which is generally satisfactory, are described.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	The 9 x 3 in. induced-flow high-speed wind tunnel at the national physical laboratory	en_US