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Showing 1 to 3 of 3 for “"Minimum induced loss."”.

  1. Aerodynamic and aeroacoustic design of small unmanned aircraft system propellers at low Reynolds numbers.

    … tested. A Prandtl bell-shaped lift distribution, minimum induced loss design, was applied to a propeller resulting in decreased power consumption and improved electrical efficiency by 18.51% with a SPL reduction of 11.15 dBA compared against the Baseline propeller. The Baseline propeller used an …

    tdl Repository record for Aerodynamic and aeroacoustic design of small unmanned aircraft system propellers at low Reynolds numbers. (opens in a new tab)

  2. Design of a Low Reynolds Number Propulsion System for an Autonomous Underwater Vehicle

    … The methodology consists of determining the minimum induced loss lift distribution for the propeller via lifting line theory, efficient airfoil sections for the propeller via a coupled viscous-inviscid flow solver and optimization, brushless DC motor identification via ideal motor theory and …

    vt Repository record for Design of a Low Reynolds Number Propulsion System for an Autonomous Underwater Vehicle (opens in a new tab)

  3. Rotor Wakes; Formations, Interactions, and Design

    … using a vortex filament in its place. The minimum induced loss (MIL) rotor has long served as the conventional baseline in rotor design. However, with the rise of DEP configurations, blown-wing systems, urban air mobility, and the widespread use of drones in populated environments, rotor …

    uiuc Repository record for Rotor Wakes; Formations, Interactions, and Design (opens in a new tab)