Addendum to type record. Avro "Lancaster" Mk.1 P. A. 474 Type record No. 1/P1/Lancaster. Investigation of boundary layer conditions on wings. M.O.S. Contract No.6/Aircraft/9807/C. B. 6(a)

College of Aeronautics, Department of Aircraft Design

dc.contributor.author	College of Aeronautics, Department of Aircraft Design
dc.date.accessioned	2016-08-17T09:25:29Z
dc.date.available	2016-08-17T09:25:29Z
dc.date.issued	1956-01
dc.identifier.uri	http://dspace.lib.cranfield.ac.uk/handle/1826/10328
dc.description.abstract	Introduction The investigation involves, briefly, the mounting of a wing of 45' sweep-back in a dorsal position on the fuselage of 'Lancaster' P.A.474 such that wing incidence will be variable in flight over a 20 range, i.e. ± 100. A ‘partial chord’ technique for swept wings has been established by the College using a similar wing mounting configuration on an Avro 'Anson' Aircraft and this technique has been applied to the current investigation.	en_UK
dc.language.iso	en	en_UK
dc.publisher	College of Aeronautics	en_UK
dc.title	Addendum to type record. Avro "Lancaster" Mk.1 P. A. 474 Type record No. 1/P1/Lancaster. Investigation of boundary layer conditions on wings. M.O.S. Contract No.6/Aircraft/9807/C. B. 6(a)	en_UK
dc.type	Report	en_UK