Aerodynamic design of a multi-purpose miocro-UAV airframe

Authors

  • Aleksandr Borisovich Ayrapetov
  • Andrey Vladimirovich Katunin FGUP CAGI
  • Aleksey Muhammetovich Timerbulatov

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.

Published

2019-04-07

Issue

Section

AIRCRAFT AND ROCKET AND SPACE TECHNOLOGY