Power required for given total drag force Calculator

✖Drag Force is the resisting force experienced by an object moving through a fluid.ⓘ Drag Force [F_D]			+10% -10%
✖The Freestream Velocity is the velocity of air far upstream of an aerodynamic body, that is before the body has a chance to deflect, slow down or compress the air.ⓘ Freestream Velocity [V_∞]			+10% -10%

✖Power is defined as the product of thrust force and velocity of aircraft.ⓘ Power required for given total drag force [P]

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Power required for given total drag force Solution

STEP 0: Pre-Calculation Summary

Formula Used

Power = Drag Force*Freestream Velocity
P = F_D*V_∞
This formula uses 3 Variables

Variables Used

Power - (Measured in Watt) - Power is defined as the product of thrust force and velocity of aircraft.
Drag Force - (Measured in Newton) - Drag Force is the resisting force experienced by an object moving through a fluid.
Freestream Velocity - (Measured in Meter per Second) - The Freestream Velocity is the velocity of air far upstream of an aerodynamic body, that is before the body has a chance to deflect, slow down or compress the air.

STEP 1: Convert Input(s) to Base Unit

Drag Force: 99.99 Newton --> 99.99 Newton No Conversion Required
Freestream Velocity: 30 Meter per Second --> 30 Meter per Second No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

P = F_D*V_∞ --> 99.99*30

Evaluating ... ...

P = 2999.7

STEP 3: Convert Result to Output's Unit

2999.7 Watt --> No Conversion Required

FINAL ANSWER

2999.7 Watt <-- Power

(Calculation completed in 00.004 seconds)

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Created by Vinay Mishra

Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune

Vinay Mishra has created this Calculator and 300+ more calculators!

Verified by Maiarutselvan V

PSG College of Technology (PSGCT), Coimbatore

Maiarutselvan V has verified this Calculator and 300+ more calculators!

< Thrust and Power Requirements Calculators

Thrust Angle for Unaccelerated Level Flight for given Lift

LaTeX Go Thrust Angle = asin((Weight of Body-Lift Force)/Thrust)

Weight of Aircraft in Level, Unaccelerated Flight

LaTeX Go Weight of Body = Lift Force+(Thrust*sin(Thrust Angle))

Thrust for Level and Unaccelerated Flight

LaTeX Go Thrust = Drag Force/(cos(Thrust Angle))

Thrust Angle for Unaccelerated Level Flight for given Drag

LaTeX Go Thrust Angle = acos(Drag Force/Thrust)

Power required for given total drag force Formula

LaTeX Go

Power = Drag Force*Freestream Velocity
P = F_D*V_∞

What is the condition for steady, level flight?

In all cases, for all engines, when the aircraft is in equilibrium at steady level flight, thrust equals drag.

How to Calculate Power required for given total drag force?

Power required for given total drag force calculator uses Power = Drag Force*Freestream Velocity to calculate the Power, The Power required for given total drag force refers to the amount of mechanical energy needed to maintain the motion or performance of a system, the power required is primarily used to overcome aerodynamic drag, which is the resistance encountered by the aircraft as it moves through the air. Power is denoted by P symbol.

How to calculate Power required for given total drag force using this online calculator? To use this online calculator for Power required for given total drag force, enter Drag Force (F_D) & Freestream Velocity (V_∞) and hit the calculate button. Here is how the Power required for given total drag force calculation can be explained with given input values -> 2999.7 = 99.99*30.

FAQ

What is Power required for given total drag force?

The Power required for given total drag force refers to the amount of mechanical energy needed to maintain the motion or performance of a system, the power required is primarily used to overcome aerodynamic drag, which is the resistance encountered by the aircraft as it moves through the air and is represented as P = F_D*V_∞ or Power = Drag Force*Freestream Velocity. Drag Force is the resisting force experienced by an object moving through a fluid & The Freestream Velocity is the velocity of air far upstream of an aerodynamic body, that is before the body has a chance to deflect, slow down or compress the air.

How to calculate Power required for given total drag force?

The Power required for given total drag force refers to the amount of mechanical energy needed to maintain the motion or performance of a system, the power required is primarily used to overcome aerodynamic drag, which is the resistance encountered by the aircraft as it moves through the air is calculated using Power = Drag Force*Freestream Velocity. To calculate Power required for given total drag force, you need Drag Force (F_D) & Freestream Velocity (V_∞). With our tool, you need to enter the respective value for Drag Force & Freestream Velocity and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

How many ways are there to calculate Power?

In this formula, Power uses Drag Force & Freestream Velocity. We can use 2 other way(s) to calculate the same, which is/are as follows -

Power = Freestream Velocity*Thrust
Power = Weight of Body*Freestream Velocity*Drag Coefficient/Lift Coefficient

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