000001596 001__ 1596
000001596 005__ 20141118153501.0
000001596 04107 $$acze
000001596 046__ $$k2007-05-14
000001596 100__ $$aČečrdle, J.
000001596 24500 $$aOPTIMIZATION OF THE COMMUTER AIRCRAFT WING STIFFNESS CHARACTERISTICS CONSIDERING REQUIREMENT OF AEROELASTIC STABILITY AT THE CERTIFICATION SPEED

000001596 24630 $$n13$$pEngineering Mechanics 2007
000001596 260__ $$bInstitute of Thermomechanics AS CR, v.v.i., Prague
000001596 506__ $$arestricted
000001596 520__ $$2eng$$aThe submitted paper deals with aeroelastic optimization. It gives a summary of theory with special regard to the aeroelasticity. Main part describes optimization of the aircraft wing stiffness characteristics to ensure the flutter stability below the certification speed. The problem is represented by the wing tip tank filling, which causes significant change of the modal characteristics and so the flutter stability characteristics. The task aim is to ensure flutter stability below the certification speed for whole range of the tip tank filling.

000001596 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000001596 653__ $$a

000001596 7112_ $$aEngineering Mechanics 2007$$cSvratka (CZ)$$d2007-05-14 / 2007-05-17$$gEM2007
000001596 720__ $$aČečrdle, J.
000001596 8560_ $$ffischerc@itam.cas.cz
000001596 8564_ $$s2033811$$uhttps://invenio.itam.cas.cz/record/1596/files/011-Cecrdle-PT.pdf$$y
             Original version of the author's contribution as presented on CD, .
            
000001596 962__ $$r1585
000001596 980__ $$aPAPER