A resume of maximum lift data for symmetrical wings, with various high-lift aids
| dc.contributor.author | Nonweiler, T. | |
| dc.date.accessioned | 2016-12-07T12:41:44Z | |
| dc.date.available | 2016-12-07T12:41:44Z | |
| dc.date.issued | 1954-03 | |
| dc.description.abstract | We shall attempt here to summarise the existing data on the values of the low-speed CLmax of wings, in the absence of a fuselage, and without including information on stalling incidence or pitching moment. The summary is limited to the consideration of unswept wings, and those of delta planforms, which have symmetrical sections: there is some discussion of the maximum lift increments due to the use of flaps of various kinds. | en_UK |
| dc.identifier.uri | http://dspace.lib.cranfield.ac.uk/handle/1826/11103 | |
| dc.language.iso | en | en_UK |
| dc.publisher | College of Aeronautics | en_UK |
| dc.relation.ispartofseries | CoA/N-5 | en_UK |
| dc.relation.ispartofseries | 5 | en_UK |
| dc.title | A resume of maximum lift data for symmetrical wings, with various high-lift aids | en_UK |
| dc.type | Report | en_UK |