Measurements of Aerodynamic Interference of a Hybrid Aircraft with Multirotor Propulsion

Measurements of Aerodynamic Interference of a Hybrid Aircraft with Multirotor Propulsion

Blog Article

This article deals with the phenomenon of aerodynamic interference occurring in the innovative hybrid system of multirotor aircraft propulsion.The approach to aerodynamics requires a determination of the impact of active sources of lift and thrust upon the aircraft aerodynamic characteristics.The hybrid propulsion unit, composed of a conventional multirotor source of thrust as well as lift in the form of the main rotor and a pusher, primera mano tequila was equipped with an additional propeller drive unit.The tests were conducted in a continuous-flow low speed wind tunnel with an open measuring space, 1.

5 m in diameter and 2.0 m long.Force testing made it possible to develop aerodynamic characteristics as well as defining aerodynamic characteristics and defining the field of speed for hp 15-ef1005ds the considered design configurations.Our investigations enabled us to analyze the results in terms of a mutual impact of particular components of the research object and the area of impact of active elements present in a common flow.