Lift Force Calculator

✖The Lift Coefficient is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area.ⓘ Lift Coefficient [C_L]			+10% -10%
✖Dynamic Pressure is simply a convenient name for the quantity which represents the decrease in the pressure due to the velocity of the fluid.ⓘ Dynamic Pressure [q]			+10% -10%
✖Area For Flow decreases velocity increases and vice versa. For subsonic flows, M < 1, the behavior resembles that for incompressible flows.ⓘ Area For Flow [A]			+10% -10%

✖The Lift Force, lifting force or simply lift is the sum of all the forces on a body that force it to move perpendicular to the direction of flow.ⓘ Lift Force [F_L]

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Lift Force Solution

STEP 0: Pre-Calculation Summary

Formula Used

Lift Force = Lift Coefficient*Dynamic Pressure*Area For Flow
F_L = C_L*q*A
This formula uses 4 Variables

Variables Used

Lift Force - (Measured in Newton) - The Lift Force, lifting force or simply lift is the sum of all the forces on a body that force it to move perpendicular to the direction of flow.
Lift Coefficient - The Lift Coefficient is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area.
Dynamic Pressure - (Measured in Pascal) - Dynamic Pressure is simply a convenient name for the quantity which represents the decrease in the pressure due to the velocity of the fluid.
Area For Flow - (Measured in Square Meter) - Area For Flow decreases velocity increases and vice versa. For subsonic flows, M < 1, the behavior resembles that for incompressible flows.

STEP 1: Convert Input(s) to Base Unit

Lift Coefficient: 0.021 --> No Conversion Required
Dynamic Pressure: 10 Pascal --> 10 Pascal No Conversion Required
Area For Flow: 50 Square Meter --> 50 Square Meter No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

F_L = C_L*q*A --> 0.021*10*50

Evaluating ... ...

F_L = 10.5

STEP 3: Convert Result to Output's Unit

10.5 Newton --> No Conversion Required

FINAL ANSWER

10.5 Newton <-- Lift Force

(Calculation completed in 00.004 seconds)

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Created by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

Sanjay Krishna has created this Calculator and 300+ more calculators!

Verified by Rushi Shah

K J Somaiya College of Engineering (K J Somaiya), Mumbai

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< Hypersonic Flow Parameters Calculators

Coefficient of Pressure with Similarity Parameters

LaTeX Go Pressure Coefficient = 2*Flow Deflection angle^2*((Specific Heat Ratio+1)/4+sqrt(((Specific Heat Ratio+1)/4)^2+1/Hypersonic Similarity Parameter^2))

Deflection Angle

LaTeX Go Deflection Angle = 2/(Specific Heat Ratio-1)*(1/Mach Number ahead of Shock-1/Mach Number Behind Shock)

Coefficient of Drag

LaTeX Go Drag Coefficient = Drag Force/(Dynamic Pressure*Area For Flow)

Axial Force Coefficient

LaTeX Go Coefficient of Force = Force/(Dynamic Pressure*Area For Flow)

Lift Force Formula

LaTeX Go

Lift Force = Lift Coefficient*Dynamic Pressure*Area For Flow
F_L = C_L*q*A

Calculating the lift force acting on the body

A fluid flowing around the surface of an object exerts a force on it. Lift is the component of this force that is perpendicular to the oncoming flow direction. It contrasts with the drag force, which is the component of the force parallel to the flow direction.

How to Calculate Lift Force?

Lift Force calculator uses Lift Force = Lift Coefficient*Dynamic Pressure*Area For Flow to calculate the Lift Force, Lift Force formula is defined as a measure of the upward force exerted on an object as it moves through a fluid, such as air or water, at high velocities, particularly in the context of hypersonic flow parameters, where the interaction between the object and the fluid is critical. Lift Force is denoted by F_L symbol.

How to calculate Lift Force using this online calculator? To use this online calculator for Lift Force, enter Lift Coefficient (C_L), Dynamic Pressure (q) & Area For Flow (A) and hit the calculate button. Here is how the Lift Force calculation can be explained with given input values -> 550 = 0.021*10*50.

FAQ

What is Lift Force?

Lift Force formula is defined as a measure of the upward force exerted on an object as it moves through a fluid, such as air or water, at high velocities, particularly in the context of hypersonic flow parameters, where the interaction between the object and the fluid is critical and is represented as F_L = C_L*q*A or Lift Force = Lift Coefficient*Dynamic Pressure*Area For Flow. The Lift Coefficient is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area, Dynamic Pressure is simply a convenient name for the quantity which represents the decrease in the pressure due to the velocity of the fluid & Area For Flow decreases velocity increases and vice versa. For subsonic flows, M < 1, the behavior resembles that for incompressible flows.

How to calculate Lift Force?

Lift Force formula is defined as a measure of the upward force exerted on an object as it moves through a fluid, such as air or water, at high velocities, particularly in the context of hypersonic flow parameters, where the interaction between the object and the fluid is critical is calculated using Lift Force = Lift Coefficient*Dynamic Pressure*Area For Flow. To calculate Lift Force, you need Lift Coefficient (C_L), Dynamic Pressure (q) & Area For Flow (A). With our tool, you need to enter the respective value for Lift Coefficient, Dynamic Pressure & Area For Flow and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

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