000001396 001__ 1396
000001396 005__ 20141118153508.0
000001396 04107 $$acze
000001396 046__ $$k2003-05-12
000001396 100__ $$aDaněk, V.
000001396 24500 $$aInfluence of cross-coupling on aircraft dynamic stability

000001396 24630 $$n9.$$pEngineering Mechanics 2003
000001396 260__ $$bInstitute of Theoretical and Applied Mechanics AS CR, Prague
000001396 506__ $$arestricted
000001396 520__ $$2eng$$aThe stability of the asymmetric flight regimes, where the couplings between longitudinal and lateral aerodynamic characteristics are significantly influencing each other, is investigated here. The system matrix is enlarged by the coupling matrices. In the coupling matrices. and basic matrices., the influence of the roll angle and the side-slip angle is included. The built-up computational model was applied for investigating the dynamic stability with six degrees of freedom at the real aeroplane, where the mutual strong aerodynamic couplings of longitudinal and lateral-directional motions, caused by the interference between wing and fuselage, were demonstrated by the results from the tunnel tests. The influence of propeller and engine rotate parts of gyroscopic effect is ignored.

000001396 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000001396 653__ $$a

000001396 7112_ $$aEngineering Mechanics 2003$$cSvratka (CZ)$$d2003-05-12 / 2003-05-15$$gEM2003
000001396 720__ $$aDaněk, V.
000001396 8560_ $$ffischerc@itam.cas.cz
000001396 8564_ $$s219448$$uhttp://invenio.itam.cas.cz/record/1396/files/117-Vladimir-Danek-PT.pdf$$y
             Original version of the author's contribution as presented on CD, DYN.
            
000001396 962__ $$r971
000001396 980__ $$aPAPER