000000817 001__ 817
000000817 005__ 20141118153515.0
000000817 04107 $$acze
000000817 046__ $$k2002-05-13
000000817 100__ $$aDaněk, V.
000000817 24500 $$aPOČETNÍ A EXPERIMENTÁLNÍ STANOVENÍ CHARAKTERISTIK PODÉLNÉ OVLADATELNOSTI LETADLA
000000817 24630 $$n8.$$pEngineering Mechanics 2002
000000817 260__ $$bInstitute of Mechanics and Solids, FME, TU Brno
000000817 506__ $$arestricted
000000817 520__ $$2cze$$aAbstrakt: The results oj computational estimations oj deviation histories oj aircraft pitching control in dependence on jlight regime at steady horizontal jlight are presented here. These results are compared with those obtained Jrom jlight measurements. Mentioned characteristics belong to the important criteria monitored Jor the considering oj the longitudinal aircraft manoeuvrability. The aim was to verifý the accuracy oj computational estimations experimentally. For the purpose relatively simple and inexpensive jlight measurements, done with a motor glider used as jlying laboratory, were perJormed. The measurements, necessary to set the aerodynamic correction oj airspeed system and the pitching control system gearing oj a motor glider, were done beJore the proper measurements oj aircraft longitudinal manoeuvrability characteristics. The computational estimations oj monitored characteristic oj motor glider longitudinal manoeuvrability were carried out with the minimum oj simplified conditions. The computation oj necessary aerodynamic characteristics oj a motor glider was done according to the available methodology, modified Jor this aircraft type. Obtained results are the basis Jor the computational model specifications Jor solution oj the jlight mechanics inverse tasks applied Jor aircraft design. aeronautika, letadlo, aerodynamika, mechanika letu, řiditelnost letounu, podélná ovladatelnost.
000000817 520__ $$2eng$$aAbstract: The results oj computational estimations oj deviation histories oj aircraft pitching control in dependence on jlight regime at steady horizontal jlight are presented here. These results are compared with those obtained Jrom jlight measurements. Mentioned characteristics belong to the important criteria monitored Jor the considering oj the longitudinal aircraft manoeuvrability. The aim was to verifý the accuracy oj computational estimations experimentally. For the purpose relatively simple and inexpensive jlight measurements, done with a motor glider used as jlying laboratory, were perJormed. The measurements, necessary to set the aerodynamic correction oj airspeed system and the pitching control system gearing oj a motor glider, were done beJore the proper measurements oj aircraft longitudinal manoeuvrability characteristics. The computational estimations oj monitored characteristic oj motor glider longitudinal manoeuvrability were carried out with the minimum oj simplified conditions. The computation oj necessary aerodynamic characteristics oj a motor glider was done according to the available methodology, modified Jor this aircraft type. Obtained results are the basis Jor the computational model specifications Jor solution oj the jlight mechanics inverse tasks applied Jor aircraft design. aeronautika, letadlo, aerodynamika, mechanika letu, řiditelnost letounu, podélná ovladatelnost.
000000817 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000000817 7112_ $$aEngineering Mechanics 2002$$cSvratka (CZ)$$d2002-05-13 / 2002-05-16$$gEM2002
000000817 720__ $$aDaněk, V.
000000817 8560_ $$ffischerc@itam.cas.cz
000000817 8564_ $$s223275$$uhttps://invenio.itam.cas.cz/record/817/files/Danek_V.pdf$$y
             Original version of the author's contribution as presented on CD, .
            
000000817 962__ $$r451
000000817 980__ $$aPAPER