An extension of Multhopp's method of calculating the spanwise loading of wing-fuselage combinations

dc.contributor.author	J. Weber	en_US
dc.contributor.author	D. A. Kirby	en_US
dc.contributor.author	D. J. Kettle	en_US
dc.date.accessioned	2014-10-21T15:53:20Z
dc.date.available	2014-10-21T15:53:20Z
dc.date.issued	1951	en_US
dc.identifier.other	ARC/R&M-2872	en_US
dc.identifier.uri	https://reports.aerade.cranfield.ac.uk/handle/1826.2/3429
dc.description.abstract	A simple method is described for calculating the spanwise loading over wing-fuselage combinations. It is based on Multhopp's method, which is extended here to cover wings of finite thickness, large root chords compared with the body diameter and also swept wings. The method is restricted to wings of moderate and large aspect ratios (above about 2). The effect of different junction shapes above and below the wing in off-centre positions of the wing cannot yet be calculated. The calculation can be performed in about one computer-day, and comparisons with experimental results show good agreement in the symmetrical case.	en_US
dc.relation.ispartofseries	Aeronautical Research Council Reports & Memoranda	en_US
dc.title	An extension of Multhopp's method of calculating the spanwise loading of wing-fuselage combinations	en_US