Aerodynamic characteristics of propeller in non-axial flow (CROSBI ID 140583)
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Podaci o odgovornosti
Vrdoljak, Milan
engleski
Aerodynamic characteristics of propeller in non-axial flow
Flow on running propellers installed on aircraft in general case is not axial what results in off-axis forces and moments at the propeller. Lifting line method is applied for propeller blade model using set of discrete vortex filaments. Propeller wake defined by vortex sheet of discrete vortex filaments is modelled with application of free-wake method. Presented propeller model combines the blade and the wake model and with its low computational cost realization it is suitable for preliminary prediction of propeller contribution to the aircraft aerodynamic characteristics.
Propeller aerodynamics; Non-axial flow; Free-wake method
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Podaci o izdanju
7 (1)
2007.
4110013-4110014
objavljeno
1617-7061
10.1002/pamm.200701078
Povezanost rada
Zrakoplovstvo, raketna i svemirska tehnika