000001754 001__ 1754
000001754 005__ 20141118153456.0
000001754 04107 $$acze
000001754 046__ $$k2010-05-10
000001754 100__ $$aČečrdle, J.
000001754 24500 $$aAssessment of aileron tab installation influence to ultra-light aircraft flutter characteristics

000001754 24630 $$n16$$pEngineering Mechanics 2010
000001754 260__ $$bInstitute of Thermomechanics AS CR, v.v.i., Prague
000001754 506__ $$arestricted
000001754 520__ $$2eng$$aSubmitted paper deals with the aileron flutter of the ultra-light aircraft. It gives an assessment of influence of the additional installation of the tab regarding the aircraft aileron flutter characteristics. The necessary actuation system stiffness and the aileron flapping frequency to ensure the stability at the aircraft maximal speed are evaluated. The work was motivated by the M-7 ultra-light aircraft accident in the western Bohemia in 2006. The FE model was prepared by the optimization approach. The design variables were mass and stiffness characteristics, design responses (constrains and objective functions) were given from the ground vibration tests data.

000001754 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000001754 653__ $$a

000001754 7112_ $$aEngineering Mechanics 2010$$cSvratka (CZ)$$d2010-05-10 / 2010-05-13$$gEM2010
000001754 720__ $$aČečrdle, J.
000001754 8560_ $$ffischerc@itam.cas.cz
000001754 8564_ $$s3011023$$uhttps://invenio.itam.cas.cz/record/1754/files/Cecrdle-088-PT.pdf$$y
             Original version of the author's contribution as presented on CD, DYN.
            
000001754 962__ $$r1750
000001754 980__ $$aPAPER