In this work elevator effectiveness for tandem-scheme aircraft (unmanned aerial vehicle or piloted one) is considered. Presented mathematical models take into account the changing of zero-lift pitching moment coefficient and wing-wing aerodynamic interference. It allows choosing geometrical parameters of flight controls for aircraft under design.
Tandem-Scheme Aircraft Controllability
01.10.2019
412556 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Simulation Analysis of the Controllability of a Tandem Ducted Fan Aircraft
British Library Conference Proceedings | 2008
|AIAA | 2016
|Calculating Aircraft Controllability Quality
NTIS | 1979
|Stability and Controllability of Supersonic Aircraft
NTIS | 1970
|