The theoretical wave drag at zero lift of fully-tapered swept wings of arbitrary section
| dc.contributor.author | Nonweiler, T. | |
| dc.date.accessioned | 2012-09-11T14:58:04Z | |
| dc.date.available | 2012-09-11T14:58:04Z | |
| dc.date.issued | 1953-10 | |
| dc.description.abstract | 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 … | en_UK |
| dc.identifier.uri | http://dspace.lib.cranfield.ac.uk/handle/1826/7564 | |
| dc.language.iso | en | en_UK |
| dc.publisher | College of Aeronautics, Cranfield | en_UK |
| dc.relation.ispartofseries | College Reports | en_UK |
| dc.relation.ispartofseries | 76 | en_UK |
| dc.title | The theoretical wave drag at zero lift of fully-tapered swept wings of arbitrary section | en_UK |
| dc.type | Report | en_UK |