Design point analysis of a distributed propulsion system with boundary layer ingestion implemented in UAV's for agriculture in the Andean region

Abstract:

∆ Pin Pressure losses at the intake FN Thrust required PW Power required TQ Torque required δ Boundary layer thickness, dimensionless correction for temperature θ Dimensionless correction for pressure ηp Propulsive efficiency Vinfty Air velocity at the intake Vj Air velocity at the exit fan ESC Electronic speed controller PWesc Electronic speed controller power PWm Electric motor power PWcom Communication power PWµC Communication power GP S Global position system IMU Inertial measurement unit

Año de publicación:

2016

Keywords:

Fuente:

google