| dc.creator | Nonweiler, T. | |
| dc.date | 2016-12-07T12:41:44Z | |
| dc.date | 2016-12-07T12:41:44Z | |
| dc.date | 1954-03 | |
| dc.date.accessioned | 2022-05-09T10:07:02Z | |
| dc.date.available | 2022-05-09T10:07:02Z | |
| dc.identifier | http://dspace.lib.cranfield.ac.uk/handle/1826/11103 | |
| dc.identifier.uri | https://reports.aerade.cranfield.ac.uk/handle/1826.2/4391 | |
| dc.description | 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. | |
| dc.language | en | |
| dc.publisher | College of Aeronautics | |
| dc.relation | CoA/N-5 | |
| dc.relation | 5 | |
| dc.title | A resume of maximum lift data for symmetrical wings, with various high-lift aids | |
| dc.type | Report |
| Files | Size | Format | View |
|---|---|---|---|
| COA_N_5_1954.pdf | 4.623Mb | application/pdf |
View/ |