| dc.creator |
Nonweiler, T. |
|
| dc.date |
2012-09-11T14:58:04Z |
|
| dc.date |
2012-09-11T14:58:04Z |
|
| dc.date |
1953-10 |
|
| dc.date.accessioned |
2022-05-09T10:17:21Z |
|
| dc.date.available |
2022-05-09T10:17:21Z |
|
| dc.identifier |
http://dspace.lib.cranfield.ac.uk/handle/1826/7564 |
|
| dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/4747 |
|
| dc.description |
An expression is deduced for the wave drag of a fully tapered swept wing of arbitrary section in the convenient form of a double integral involving the variation of wing-surface slope. It is concluded, in the general case, that the drag may best be computed by numerical integration, the method for which will be the subject of a further report. Continues … |
|
| dc.language |
en |
|
| dc.publisher |
College of Aeronautics, Cranfield |
|
| dc.relation |
College Reports |
|
| dc.relation |
76 |
|
| dc.title |
The theoretical wave drag at zero lift of fully-tapered swept wings of arbitrary section |
|
| dc.type |
Report |
|