The flexure-torsion flutter of cambered aerofoils in cascade
| dc.contributor.author | Craven, A. H. | |
| dc.date.accessioned | 2013-05-17T15:53:18Z | |
| dc.date.available | 2013-05-17T15:53:18Z | |
| dc.date.issued | 1955-12 | |
| dc.description.abstract | This report contains the results of a series of tests on the flexure-torsion flutter of cascades of aerofoils of 30° and 45° camber. The critical flutter speeds and frequencies in cascade are expressed as ratios of the values for the aerofoil in the isolated condition, The tests cover stagger angles between -30° and +30° and gap chord ratios up to 1.5 at a Reynolds number of 1 x 10 to the power of 5 based on aerofoil chord. | en_UK |
| dc.identifier.uri | http://dspace.lib.cranfield.ac.uk/handle/1826/7912 | |
| dc.language.iso | en | en_UK |
| dc.publisher | College of Aeronautics, Cranfield. | en_UK |
| dc.relation.ispartofseries | College Report | en_UK |
| dc.relation.ispartofseries | 95 | en_UK |
| dc.title | The flexure-torsion flutter of cambered aerofoils in cascade | en_UK |
| dc.type | Report | en_UK |