| dc.creator |
Craven, A. H. |
|
| dc.date |
2013-05-17T15:53:18Z |
|
| dc.date |
2013-05-17T15:53:18Z |
|
| dc.date |
1955-12 |
|
| dc.date.accessioned |
2022-05-09T10:17:22Z |
|
| dc.date.available |
2022-05-09T10:17:22Z |
|
| dc.identifier |
http://dspace.lib.cranfield.ac.uk/handle/1826/7912 |
|
| dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/4769 |
|
| dc.description |
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. |
|
| dc.language |
en |
|
| dc.publisher |
College of Aeronautics, Cranfield. |
|
| dc.relation |
College Report |
|
| dc.relation |
95 |
|
| dc.title |
The flexure-torsion flutter of cambered aerofoils in cascade |
|
| dc.type |
Report |
|