Lift given lift coefficient Calculator

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✖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, also referred to as velocity pressure, is a specific type of pressure associated with the kinetic energy per unit volume of a moving fluid.ⓘ Dynamic Pressure [q]			+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 lift coefficient [F_L]

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Formula

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Lift given lift coefficient

Formula

`"F"_{"L"} = "C"_{"L"}*"q"`

Example

`"11N"="1.1"*"10Pa"`

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Lift given lift coefficient Solution

STEP 0: Pre-Calculation Summary

Formula Used

Lift Force = Lift Coefficient*Dynamic Pressure
F_L = C_L*q
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.
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, also referred to as velocity pressure, is a specific type of pressure associated with the kinetic energy per unit volume of a moving fluid.

STEP 1: Convert Input(s) to Base Unit

Lift Coefficient: 1.1 --> No Conversion Required
Dynamic Pressure: 10 Pascal --> 10 Pascal No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

F_L = C_L*q --> 1.1*10

Evaluating ... ...

F_L = 11

STEP 3: Convert Result to Output's Unit

11 Newton --> No Conversion Required

FINAL ANSWER

11 Newton <-- Lift Force

(Calculation completed in 00.004 seconds)

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Created by Himanshu Sharma

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

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National Institute Of Technology (NIT), Hamirpur

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< 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 lift coefficient Formula

Lift Force = Lift Coefficient*Dynamic Pressure
F_L = C_L*q

What is lift?

A fluid flowing around 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 given lift coefficient?

Lift given lift coefficient calculator uses Lift Force = Lift Coefficient*Dynamic Pressure to calculate the Lift Force, The Lift given lift coefficient formula is defined as amount of lift generated for the aircraft inducing the dynamic pressure and that of the lift coefficient given. Lift Force is denoted by F_L symbol.

How to calculate Lift given lift coefficient using this online calculator? To use this online calculator for Lift given lift coefficient, enter Lift Coefficient (C_L) & Dynamic Pressure (q) and hit the calculate button. Here is how the Lift given lift coefficient calculation can be explained with given input values -> 11 = 1.1*10.

FAQ

What is Lift given lift coefficient?

The Lift given lift coefficient formula is defined as amount of lift generated for the aircraft inducing the dynamic pressure and that of the lift coefficient given and is represented as F_L = C_L*q or Lift Force = Lift Coefficient*Dynamic Pressure. 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, also referred to as velocity pressure, is a specific type of pressure associated with the kinetic energy per unit volume of a moving fluid.

How to calculate Lift given lift coefficient?

The Lift given lift coefficient formula is defined as amount of lift generated for the aircraft inducing the dynamic pressure and that of the lift coefficient given is calculated using Lift Force = Lift Coefficient*Dynamic Pressure. To calculate Lift given lift coefficient, you need Lift Coefficient (C_L) & Dynamic Pressure (q). With our tool, you need to enter the respective value for Lift Coefficient & Dynamic Pressure 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 Lift Coefficient & Dynamic Pressure. We can use 3 other way(s) to calculate the same, which is/are as follows -

Lift Force = Lift Coefficient/Drag Coefficient*Drag Force
Lift Force = Aerodynamic Force-Drag Force
Lift Force = sqrt(Induced Drag*3.14*Dynamic Pressure*Lateral plane span^2)

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