Lift given aerodynamic force Solution

STEP 0: Pre-Calculation Summary
Formula Used
Lift Force = Aerodynamic Force-Drag Force
FL = F-FD
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: 134 Newton --> 134 Newton No Conversion Required
Drag Force: 80 Newton --> 80 Newton No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
FL = F-FD --> 134-80
Evaluating ... ...
FL = 54
STEP 3: Convert Result to Output's Unit
54 Newton --> No Conversion Required
FINAL ANSWER
54 Newton <-- Lift Force
(Calculation completed in 00.004 seconds)

Credits

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
Kartikay Pandit has verified this Calculator and 400+ more calculators!

21 Lift and Drag Polar Calculators

Drag Coefficient for given zero-lift drag coefficient
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
Go Drag Coefficient = Parasite Drag coefficient+((Lift Coefficient^2)/(pi*Oswald Efficiency Factor*Aspect Ratio of a wing))
Coefficient of Drag due to lift
Go Coefficient of drag due to lift = (Lift Coefficient^2)/(pi*Oswald Efficiency Factor*Aspect Ratio of a wing)
Modern Lift Equation
Go Lift on Airfoil = (Lift Coefficient*Air Density*Aircraft Gross Wing Area*Fluid Velocity^2)/2
Induced drag given span efficiency factor
Go Induced Drag = Drag Coefficient*Density of Material*Velocity^2*Reference Area/2
Lift given induced drag
Go Lift Force = sqrt(Induced Drag*3.14*Dynamic Pressure*Lateral plane span^2)
Induced Drag for Wings having Elliptic Lift Distribution
Go Induced Drag = (Lift Force^2)/(3.14*Dynamic Pressure*Lateral plane span^2)
Coefficient of lift given drag
Go Lift Coefficient = (Gross Weight*Drag Coefficient)/Drag Force
Coefficient of drag given drag
Go Drag Coefficient = (Lift Coefficient*Drag Force)/Gross Weight
Drag
Go Drag Force = Gross Weight/Lift Coefficient/Drag Coefficient
Lift coefficient given drag coefficient
Go Lift Coefficient = Lift Force/Drag Force*Drag Coefficient
Drag coefficient given lift coefficient
Go Drag Coefficient = Lift Coefficient*Drag Force/Lift Force
Lift given drag coefficient
Go Lift Force = Lift Coefficient/Drag Coefficient*Drag Force
Drag given lift coefficient
Go Drag Force = Lift Force*Drag Coefficient/Lift Coefficient
Parasite Drag Coefficient at zero lift
Go Zero-lift drag coefficient = Drag Coefficient-Coefficient of drag due to lift
Lift given lift coefficient
Go Lift Force = Lift Coefficient*Dynamic Pressure
Drag given drag coefficient
Go Drag Force = Drag Coefficient*Dynamic Pressure
Lift coefficient new
Go Lift Coefficient = Lift Force/Dynamic Pressure
Drag coefficient new
Go Drag Coefficient = Drag Force/Dynamic Pressure
Lift given aerodynamic force
Go Lift Force = Aerodynamic Force-Drag Force
Drag given aerodynamic force
Go Drag Force = Aerodynamic Force-Lift Force

Lift given aerodynamic force Formula

Lift Force = Aerodynamic Force-Drag Force
FL = F-FD

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, The Lift given aerodynamic force formula is defined as amount of lift produced to define the relative motion between body and gas. Lift Force is denoted by FL 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 (FD) and hit the calculate button. Here is how the Lift given aerodynamic force calculation can be explained with given input values -> 54 = 134-80.

FAQ

What is Lift given aerodynamic force?
The Lift given aerodynamic force formula is defined as amount of lift produced to define the relative motion between body and gas and is represented as FL = F-FD 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?
The Lift given aerodynamic force formula is defined as amount of lift produced to define the relative motion between body and gas is calculated using Lift Force = Aerodynamic Force-Drag Force. To calculate Lift given aerodynamic force, you need Aerodynamic Force (F) & Drag Force (FD). 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)
Let Others Know
Facebook
Twitter
Reddit
LinkedIn
Email
WhatsApp
Copied!