Aerodynamic design of a multi-purpose miocro-UAV airframe
Keywords:
miocro-UAV; aerodinamics; low Reynolds numbers; flying wing.Abstract
The rationale for the selection and aerodynamic design of the miocro-UAV model are considered. The the method principles for calculating the aerodynamic characteristics of the wing profile at low Reynolds numbers are presented. Design calculations of profiles for the created model are carried out.Downloads
Published
2019-04-07
Issue
Section
AIRCRAFT AND ROCKET AND SPACE TECHNOLOGY