Induced Inflow Ratio in Hover evaluator uses Inflow Ratio = Induced Velocity/(Rotor Radius*Angular Velocity) to evaluate the Inflow Ratio, The Induced Inflow Ratio in Hover refers to the ratio of the induced velocity at the rotor disc to the velocity of the rotor tip, it quantifies the increase in airspeed induced by the rotor as it generates lift in a hovering condition, the Induced Inflow Ratio provides insights into the efficiency and effectiveness of the rotor in generating lift during hover. Inflow Ratio is denoted by λ symbol.
How to evaluate Induced Inflow Ratio in Hover using this online evaluator? To use this online evaluator for Induced Inflow Ratio in Hover, enter Induced Velocity (vi), Rotor Radius (Rrotor) & Angular Velocity (ω) and hit the calculate button.