Calculated velocity distribution and force derivatives for a series of high-speed aerofoils

dc.contributor.author	C. S. Sinnott	en_US
dc.date.accessioned	2014-10-21T15:54:18Z
dc.date.available	2014-10-21T15:54:18Z
dc.date.issued	1955	en_US
dc.identifier.other	ARC/R&M-3045	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3614
dc.description.abstract	The Polygon method of Woods is used to calculate the velocity distribution over a number of two-dimensional aerofoils at low incidence, subcritical flows only being considered. Lift slopes and aerodynamic centres at zero lift are also calculated. Some comparisons with experimental results are made, and these show good agreement at zero incidence.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Calculated velocity distribution and force derivatives for a series of high-speed aerofoils	en_US