Abstract Algorithms for determining fixed-pitch propeller parameters and some flight characteristics of a superlight aircraft at the early stage of designing are described.
Design calculation of superlight piston-engined aircraft flight characteristics
Russian Aeronautics (Iz VUZ) ; 51 , 2 ; 114-118
01.06.2008
5 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Design calculation of superlight piston-engined aircraft flight characteristics
Online Contents | 2008
|Design calculation of light piston-engined aircraft controllability and stability parameters
Springer Verlag | 2010
|Design calculation of light piston-engined aircraft controllability and stability parameters
Online Contents | 2010
|