Drag given aerodynamic force Calculator

✖Aerodynamic force is a force exerted on a body by the air in which the body is immersed, and is due to the relative motion between the body and the gas.ⓘ Aerodynamic Force [F]			+10% -10%
✖Lift force is the component of the total force acting on a body that is perpendicular to the direction of the fluid flow.ⓘ Lift Force [F_L]			+10% -10%

✖Drag Force is the resisting force experienced by an object moving through a fluid ,such as air.ⓘ Drag given aerodynamic force [F_D]

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Drag given aerodynamic force Solution

STEP 0: Pre-Calculation Summary

Formula Used

Drag Force = Aerodynamic Force-Lift Force
F_D = F-F_L
This formula uses 3 Variables

Variables Used

Drag Force - (Measured in Newton) - Drag Force is the resisting force experienced by an object moving through a fluid ,such as air.
Aerodynamic Force - (Measured in Newton) - Aerodynamic force is a force exerted on a body by the air in which the body is immersed, and is due to the relative motion between the body and the gas.
Lift Force - (Measured in Newton) - Lift force is the component of the total force acting on a body that is perpendicular to the direction of the fluid flow.

STEP 1: Convert Input(s) to Base Unit

Aerodynamic Force: 82.926 Newton --> 82.926 Newton No Conversion Required
Lift Force: 2.926 Newton --> 2.926 Newton No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

F_D = F-F_L --> 82.926-2.926

Evaluating ... ...

F_D = 80

STEP 3: Convert Result to Output's Unit

80 Newton --> No Conversion Required

FINAL ANSWER

80 Newton <-- Drag Force

(Calculation completed in 00.004 seconds)

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Home » Physics » Aircraft Mechanics » Introduction and Governing Equations » Aerospace » Lift and Drag Polar » Drag given aerodynamic force

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Created by Himanshu Sharma

National Institute of Technology, Hamirpur (NITH), Himachal Pradesh

Himanshu Sharma has created this Calculator and 50+ more calculators!

Verified by Kartikay Pandit

National Institute Of Technology (NIT), Hamirpur

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< Lift and Drag Polar Calculators

Drag Coefficient for given zero-lift drag coefficient

LaTeX Go Drag Coefficient = Zero-Lift Drag Coefficient+((Lift Coefficient^2)/(pi*Oswald Efficiency Factor*Aspect Ratio of a Wing))

Drag Coefficient for given parasite drag coefficient

LaTeX Go Drag Coefficient = Parasite Drag coefficient+((Lift Coefficient^2)/(pi*Oswald Efficiency Factor*Aspect Ratio of a Wing))

Coefficient of Drag due to lift

LaTeX Go Coefficient of Drag due to Lift = (Lift Coefficient^2)/(pi*Oswald Efficiency Factor*Aspect Ratio of a Wing)

Parasite Drag Coefficient at zero lift

LaTeX Go Zero-Lift Drag Coefficient = Drag Coefficient-Coefficient of Drag due to Lift

Drag given aerodynamic force Formula

LaTeX Go

Drag Force = Aerodynamic Force-Lift Force
F_D = F-F_L

What is drag?

Drag is an example of mechanical force. When a solid body interacts with a fluid (liquid or gas), a drag force is produced on the solid body.

How to Calculate Drag given aerodynamic force?

Drag given aerodynamic force calculator uses Drag Force = Aerodynamic Force-Lift Force to calculate the Drag Force, Drag given aerodynamic force is a measure of the horizontal force exerted on an object as it moves through a fluid, calculated by subtracting the lift force from the aerodynamic force, providing a crucial indicator of air resistance in various engineering and scientific applications. Drag Force is denoted by F_D symbol.

How to calculate Drag given aerodynamic force using this online calculator? To use this online calculator for Drag given aerodynamic force, enter Aerodynamic Force (F) & Lift Force (F_L) and hit the calculate button. Here is how the Drag given aerodynamic force calculation can be explained with given input values -> 74.148 = 82.926-2.926.

FAQ

What is Drag given aerodynamic force?

Drag given aerodynamic force is a measure of the horizontal force exerted on an object as it moves through a fluid, calculated by subtracting the lift force from the aerodynamic force, providing a crucial indicator of air resistance in various engineering and scientific applications and is represented as F_D = F-F_L or Drag Force = Aerodynamic Force-Lift Force. Aerodynamic force is a force exerted on a body by the air in which the body is immersed, and is due to the relative motion between the body and the gas & Lift force is the component of the total force acting on a body that is perpendicular to the direction of the fluid flow.

How to calculate Drag given aerodynamic force?

Drag given aerodynamic force is a measure of the horizontal force exerted on an object as it moves through a fluid, calculated by subtracting the lift force from the aerodynamic force, providing a crucial indicator of air resistance in various engineering and scientific applications is calculated using Drag Force = Aerodynamic Force-Lift Force. To calculate Drag given aerodynamic force, you need Aerodynamic Force (F) & Lift Force (F_L). With our tool, you need to enter the respective value for Aerodynamic Force & Lift Force 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 Drag Force?

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

Drag Force = Drag Coefficient*Dynamic Pressure
Drag Force = Lift Force*Drag Coefficient/Lift Coefficient

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