Finite difference solutions for an unsteady interference parameter in slotted wind tunnels

dc.contributor.author	K.R. Rushton	en_US
dc.contributor.author	Lucy M. Laing	en_US
dc.date.accessioned	2014-10-20T11:05:30Z
dc.date.available	2014-10-20T11:05:30Z
dc.date.issued	1968	en_US
dc.identifier.other	ARC/CP-1053	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/1066
dc.description.abstract	Three methods of determining an unsteady interference parameter in slotted wind tunnels are described. In each case the governing equation for the flow in the wind tunnel is Laplace’s equation which is solved by a finite difference approximation. The methods differ in the representatIon of the disturbance due to the wing. A discussion of the merits of each method is included, results are quoted for tunnels of square section with roof and floor of varying slot parameter.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Current Papers	en_US
dc.title	Finite difference solutions for an unsteady interference parameter in slotted wind tunnels	en_US