Tytuł artykułu
Autorzy
Identyfikatory
Warianty tytułu
Konferencja
Proceedings of the Fourth Seminar on Recent Research and Design Progress in Aeronautical Engineering and its Influence on Education/seminar(IV; 30.11-02.12.2000; Warszawa, Polska)
Języki publikacji
Abstrakty
A linearized analytic model of general longitudinal movement of airplane is discussed. Linearized deviation equations of motion, derived in stability axes system, are applied to the parametric analysis of airplane's longitudinal dynamic stability under arbitrary symmetric flight conditions. The analytic model is generated in the form of inter-active software package PODYST_ALFA. This is used to show the influence of some constructional and mass parameters on the longitudinal airplane motions after encountering disturbance for a chosen steady level flight.
Czasopismo
Rocznik
Tom
Strony
83--88
Opis fizyczny
Bibliogr. 5 poz., wykr.
Twórcy
autor
- Brno University of Technology, Brno, Czech Republic
Bibliografia
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-PWA3-0039-0011