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

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Lift given aerodynamic force Solution

STEP 0: Pre-Calculation Summary

Formula Used

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

Variables Used

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.
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.
Drag Force - (Measured in Newton) - Drag Force is the resisting force experienced by an object moving through a fluid ,such as air.

STEP 1: Convert Input(s) to Base Unit

Aerodynamic Force: 82.926 Newton --> 82.926 Newton No Conversion Required
Drag Force: 80 Newton --> 80 Newton No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

F_L = F-F_D --> 82.926-80

Evaluating ... ...

F_L = 2.926

STEP 3: Convert Result to Output's Unit

2.926 Newton --> No Conversion Required

FINAL ANSWER

2.926 Newton <-- Lift Force

(Calculation completed in 00.004 seconds)

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

Lift given aerodynamic force Formula

LaTeX Go

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

What is lift?

Lift is a mechanical force. It is generated by the interaction and contact of a solid body with a fluid (liquid or gas). It is not generated by a force field, in the sense of a gravitational field,or an electromagnetic field, where one object can affect another object without being in physical contact.

How to Calculate Lift given aerodynamic force?

Lift given aerodynamic force calculator uses Lift Force = Aerodynamic Force-Drag Force to calculate the Lift Force, Lift Given Aerodynamic Force is a measure of the upward force exerted on an object, such as an airplane wing, as it moves through the air, calculated by subtracting the drag force from the total aerodynamic force, allowing designers to optimize the shape and performance of aircraft and other objects that interact with air or water. Lift Force is denoted by F_L symbol.

How to calculate Lift given aerodynamic force using this online calculator? To use this online calculator for Lift given aerodynamic force, enter Aerodynamic Force (F) & Drag Force (F_D) and hit the calculate button. Here is how the Lift given aerodynamic force calculation can be explained with given input values -> -2.926 = 82.926-80.

FAQ

What is Lift given aerodynamic force?

Lift Given Aerodynamic Force is a measure of the upward force exerted on an object, such as an airplane wing, as it moves through the air, calculated by subtracting the drag force from the total aerodynamic force, allowing designers to optimize the shape and performance of aircraft and other objects that interact with air or water and is represented as F_L = F-F_D or Lift Force = Aerodynamic Force-Drag 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 & Drag Force is the resisting force experienced by an object moving through a fluid ,such as air.

How to calculate Lift given aerodynamic force?

Lift Given Aerodynamic Force is a measure of the upward force exerted on an object, such as an airplane wing, as it moves through the air, calculated by subtracting the drag force from the total aerodynamic force, allowing designers to optimize the shape and performance of aircraft and other objects that interact with air or water is calculated using Lift Force = Aerodynamic Force-Drag Force. To calculate Lift given aerodynamic force, you need Aerodynamic Force (F) & Drag Force (F_D). With our tool, you need to enter the respective value for Aerodynamic Force & Drag 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 Lift Force?

In this formula, Lift Force uses Aerodynamic Force & Drag Force. We can use 3 other way(s) to calculate the same, which is/are as follows -

Lift Force = Lift Coefficient*Dynamic Pressure
Lift Force = Lift Coefficient/Drag Coefficient*Drag Force
Lift Force = sqrt(Induced Drag*3.14*Dynamic Pressure*Lateral Plane Span^2)

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