An Analysis of the Lift Slope of Aerofoils of Small Aspect Ratio, including Fins, with Design Charts for Aerofoils and Control Surfaces

dc.contributor.author	D J Lyons And F/O P L Bisgood	en_US
dc.date.accessioned	2014-10-21T15:53:11Z
dc.date.available	2014-10-21T15:53:11Z
dc.date.issued	1945	en_US
dc.identifier.other	ARC/R&M-2308	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3399
dc.description.abstract	The analysis of R.A.E. Report No. Aero. 1840 has been extended to cover the lift slope of aerofoils of small aspect ratio and of fins in place upon an aeroplane. The charts of that report for the estimation of lifting characteristics of aerofoil controls have been included in this report with some small modifications, and those necessary for the estimation of fin and rudder lifting characteristics added. In general it is possible to estimate the lift slope of the aerofoils on an aircraft, taking account of interference effects, to within about ± 5 per cent. and control powers to within about ± 10 per cent.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	An Analysis of the Lift Slope of Aerofoils of Small Aspect Ratio, including Fins, with Design Charts for Aerofoils and Control Surfaces	en_US