Calculation of the influence of a body on the position of the aerodynamic centre of aircraft with sweptback wings

dc.contributor.author	H. Schlichting	en_US
dc.date.accessioned	2014-10-21T15:50:44Z
dc.date.available	2014-10-21T15:50:44Z
dc.date.issued	1947	en_US
dc.identifier.other	ARC/R&M-2582	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/2977
dc.description.abstract	From systematic three-component measurements of wing-body combinations with swept wings it has been found that the movement of the aerodynamic centre due to the influence of the body is greater for a swept forward than for a straight wing and less for a sweptback wing. The forward shift of the aerodynamic centre due to the body for normal wing body combinations is about 0.06c for a straight wing, about 0.12c for a 30 degrees swept forward, but about zero for a 45 degrees sweptback wing. A simple theoretical method is given for calculating this movement of the aerodynamic centre due to the influence of the body, and it is shown that the agreement with experimental results is quite good.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	Calculation of the influence of a body on the position of the aerodynamic centre of aircraft with sweptback wings	en_US