
Calculation of aerodynamic characteristics of light aircraft with distributed electric propulsion
Author(s) -
Artur V. Vlasov,
Maxim Ovdienko
Publication year - 2020
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/1560/1/012059
Subject(s) - aerodynamics , propulsion , aerospace engineering , electrically powered spacecraft propulsion , wing , automotive engineering , computer science , environmental science , mechanics , engineering , physics
This paper describes a numerical calculation method of the aerodynamic characteristic of an aircraft with distributed electric propulsion system (DEPS) taking into account influence of a blown wing. In addition, the studies of DEPS impact on aerodynamic characteristics of the light aircraft are represented.