| dc.creator |
College of Aeronautics, Department of Aircraft Design |
|
| dc.date |
2016-08-17T09:25:29Z |
|
| dc.date |
2016-08-17T09:25:29Z |
|
| dc.date |
1956-01 |
|
| dc.date.accessioned |
2022-05-09T10:17:30Z |
|
| dc.date.available |
2022-05-09T10:17:30Z |
|
| dc.identifier |
http://dspace.lib.cranfield.ac.uk/handle/1826/10328 |
|
| dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/4848 |
|
| dc.description |
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. |
|
| dc.language |
en |
|
| dc.publisher |
College of Aeronautics |
|
| 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) |
|
| dc.type |
Report |
|