How to Calculate Thrust-to-Weight Ratio given Vertical Velocity?
Thrust-to-Weight Ratio given Vertical Velocity calculator uses Thrust-to-Weight Ratio = ((Vertical Airspeed/Aircraft Velocity)+((Dynamic Pressure/Wing Loading)*(Minimum Drag Coefficient))+((Lift Induced Drag Constant/Dynamic Pressure)*(Wing Loading))) to calculate the Thrust-to-Weight Ratio, Thrust-to-Weight Ratio given Vertical Velocity provides a measure of an aircraft's ability to ascend vertically under the influence of its engines, this ratio is particularly important during vertical takeoff, hovering, or vertical landing maneuvers commonly performed by vertical takeoff and landing (VTOL) aircraft or helicopters. Thrust-to-Weight Ratio is denoted by TW symbol.
How to calculate Thrust-to-Weight Ratio given Vertical Velocity using this online calculator? To use this online calculator for Thrust-to-Weight Ratio given Vertical Velocity, enter Vertical Airspeed (Vv), Aircraft Velocity (Va), Dynamic Pressure (Pdynamic), Wing Loading (WS), Minimum Drag Coefficient (CDmin) & Lift Induced Drag Constant (k) and hit the calculate button. Here is how the Thrust-to-Weight Ratio given Vertical Velocity calculation can be explained with given input values -> 17.96714 = ((54/206)+((8/5)*(1.3))+((25/8)*(5))).