The flexure-torsion flutter of cambered aerofoils in cascade

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dc.creator Craven, A. H. 2013-05-17T15:53:18Z 2013-05-17T15:53:18Z 1955-12 2022-05-09T10:17:22Z 2022-05-09T10:17:22Z
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

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