The flexure-torsion flutter of cambered aerofoils in cascade

Craven, A. H.

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.identifier.uri	http://dspace.lib.cranfield.ac.uk/handle/1826/7912
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.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