05 - Propulsion
NUMERICAL AND EXPERIMENTAL INVESTIGATION OF COOLING CONCEPT FOR AN ELECTRIC PROPULSION SYSTEM FOR AEROBATIC AIRCRAFTS
X. Liu¹, F. Ferrari¹, L. Manfriani¹; ¹Zurich University for Applied Science, Switzerland
An aerobatic aircraft with electrical power has not yet been launched on the market.On the basis of the results of the research partner Bern University of Applied Sciences and the company MSW Aviation for the development of a highperformance electric motor for the aerobatics Votec 221, this project aims to explore new and efficient possibilities for cooling the powertrain.