The prevention of flutter of spring tabs

Show simple item record Collar, A. R. 2014-10-21T12:03:34Z 2014-10-21T12:03:34Z 1943
dc.identifier.other ARC/R&M-2034 en_US
dc.description.abstract The present report gives a correlation of the results of earlier researches into the prevention of flutter of spring tabs. The restrictions on the way in which tab mass-balance must be applied, which are given in the earlier work, are shown to be very simply derivable from the conditions necessary for the elimination of elastic and inertia couplings; and from these considerations an optimum length of tab balancing arm is deduced. The recommendations for avoidance of spring tab flutter are summarised in §9. Two Appendices deal respectively with the optimum length of arm when the aerodynamic actions are taken into account, and the relation between the results of the earlier work and the recommendations of §9. en_US
dc.language.iso en en_US
dc.publisher H. M. Stationery Office en_US
dc.relation.ispartofseries Aeronautical Research Committee Reports & Memoranda en_US
dc.title The prevention of flutter of spring tabs en_US
dc.type Technical Report en_US

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