000003427 001__ 3427
000003427 005__ 20141118153400.0
000003427 04107 $$acze
000003427 046__ $$k2006-05-15
000003427 100__ $$aČečrdle, J.
000003427 24500 $$aWhirl flutter analysis of the commuter aircraft aeroelastic model wing -- engine component

000003427 24630 $$n12.$$pENGINEERING MECHANICS 2006
000003427 260__ $$bInstitute of Theoretical and Applied Mechanics, AS CR, v.v.i., Prague
000003427 506__ $$arestricted
000003427 520__ $$2eng$$aThe submitted paper deals with whirl flutter of turboprop aircraft. It gives a summary of the airworthiness regulations requirements and the theoretical background concerning the mentioned aeroelastic phenomenon. The whirl flutter analysis was performed by means of the NASTRAN program system supported by other specialized software packages. The analysis was made on an aeroelastic model of the wing – engine component of a commuter aircraft for 40 passengers.

000003427 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000003427 653__ $$a

000003427 7112_ $$aENGINEERING MECHANICS 2006$$cSvratka (CZ)$$d2006-05-15 / 2006-05-18$$gEM2006
000003427 720__ $$aČečrdle, J.
000003427 8560_ $$ffischerc@itam.cas.cz
000003427 8564_ $$s574896$$uhttps://invenio.itam.cas.cz/record/3427/files/Cecrdle-119-PT.pdf$$y
             Original version of the author's contribution as presented on CD, , paper No. 119.
            
000003427 962__ $$r3410
000003427 980__ $$aPAPER