Experiments on laminar-flow aerofoil EQH 1260 in the William Froude national tank and the 13ft. x 9ft. and 9ft. x 7ft. wind tunnels at the National Physical Laboratory

dc.contributor.author	A. Fage	en_US
dc.contributor.author	W. S. Walker	en_US
dc.date.accessioned	2014-10-21T15:52:04Z
dc.date.available	2014-10-21T15:52:04Z
dc.date.issued	1942	en_US
dc.identifier.other	ARC/R&M-2165	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3166
dc.description.abstract	To determine Whether the flow conditions in the William Froude National Tank and the new 13 ft. x 9 ft. and 9 ft. × 7 ft. tunnels at the National Physical Laboratory are sufficiently steady to allow the properties of laminar-flow aerofoils to be investigated at high Reynolds numbers: and to obtain information on the behaviour of laminar-flow aerofoil section EQH 1260.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Experiments on laminar-flow aerofoil EQH 1260 in the William Froude national tank and the 13ft. x 9ft. and 9ft. x 7ft. wind tunnels at the National Physical Laboratory	en_US