Lift coefficient given Lift Force Calculator

✖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%
✖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%

✖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 given Lift Force [C_L]

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Formula

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Lift coefficient given Lift Force

Formula

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

Example

`"1.097113"="2.926N"/"2.667Pa"`

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Lift coefficient given Lift Force Solution

STEP 0: Pre-Calculation Summary

Formula Used

Lift Coefficient = Lift Force/Dynamic Pressure
C_L = F_L/q
This formula uses 3 Variables

Variables Used

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.
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.
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 Force: 2.926 Newton --> 2.926 Newton No Conversion Required
Dynamic Pressure: 2.667 Pascal --> 2.667 Pascal No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

C_L = F_L/q --> 2.926/2.667

Evaluating ... ...

C_L = 1.09711286089239

STEP 3: Convert Result to Output's Unit

1.09711286089239 --> No Conversion Required

FINAL ANSWER

1.09711286089239 ≈ 1.097113 <-- Lift Coefficient

(Calculation completed in 00.005 seconds)

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

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Created by Himanshu Sharma

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

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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

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

Drag Force Given Lift Coefficient

Go Drag Force = Lift Force*Drag Coefficient/Lift Coefficient

Lift given drag coefficient

Go Lift Force = Lift Coefficient/Drag Coefficient*Drag Force

Drag

Go Drag = Gross Weight/Lift Coefficient/Drag Coefficient

Parasite Drag Coefficient at zero lift

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

Lift coefficient given Lift Force

Go Lift Coefficient = Lift Force/Dynamic Pressure

Drag coefficient given Drag Force

Go Drag Coefficient = Drag Force/Dynamic Pressure

Lift given Lift Coefficient

Go Lift Force = Lift Coefficient*Dynamic Pressure

Drag given drag coefficient

Go Drag Force = Drag Coefficient*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 coefficient given Lift Force Formula

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

What is lift coefficient?

The lift coefficient (Cl) 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

How to Calculate Lift coefficient given Lift Force?

Lift coefficient given Lift Force calculator uses Lift Coefficient = Lift Force/Dynamic Pressure to calculate the Lift Coefficient, Lift coefficient given Lift Force is a dimensionless quantity that represents the lift force per unit density, velocity, and area of an object, characterizing its ability to generate an upward force perpendicular to the direction of motion, used to analyze and design aircraft, wind turbines, and other aerodynamic systems. Lift Coefficient is denoted by C_L symbol.

How to calculate Lift coefficient given Lift Force using this online calculator? To use this online calculator for Lift coefficient given Lift Force, enter Lift Force (F_L) & Dynamic Pressure (q) and hit the calculate button. Here is how the Lift coefficient given Lift Force calculation can be explained with given input values -> 1.1 = 2.926/2.667.

FAQ

What is Lift coefficient given Lift Force?

Lift coefficient given Lift Force is a dimensionless quantity that represents the lift force per unit density, velocity, and area of an object, characterizing its ability to generate an upward force perpendicular to the direction of motion, used to analyze and design aircraft, wind turbines, and other aerodynamic systems and is represented as C_L = F_L/q or Lift Coefficient = Lift Force/Dynamic Pressure. Lift force is the component of the total force acting on a body that is perpendicular to the direction of the fluid flow & 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 coefficient given Lift Force?

Lift coefficient given Lift Force is a dimensionless quantity that represents the lift force per unit density, velocity, and area of an object, characterizing its ability to generate an upward force perpendicular to the direction of motion, used to analyze and design aircraft, wind turbines, and other aerodynamic systems is calculated using Lift Coefficient = Lift Force/Dynamic Pressure. To calculate Lift coefficient given Lift Force, you need Lift Force (F_L) & Dynamic Pressure (q). With our tool, you need to enter the respective value for Lift Force & 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 Coefficient?

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

Lift Coefficient = (Gross Weight*Drag Coefficient)/Drag Force
Lift Coefficient = Lift Force/Drag Force*Drag Coefficient

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