The pressure distribution on two-dimensional wings near the ground

dc.contributor.author	J. A. Bagley	en_US
dc.date.accessioned	2014-10-21T15:55:30Z
dc.date.available	2014-10-21T15:55:30Z
dc.date.issued	1960	en_US
dc.identifier.other	ARC/R&M-3238	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3812
dc.description.abstract	A simple method of calculating the pressure distribution in incompressible flow on two-dimensional aerofoils of arbitrary section at moderate distances from the ground is developed. Comparisons with an 'exact' potential-flow solution, and with measurements on a 10 per cent thick aerofoil of RAE 101 section, provide a satisfactory verification of the adequacy of the method; but it is shown that it is necessary to take account of the boundary layer on the aerofoil in the calculations.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	The pressure distribution on two-dimensional wings near the ground	en_US