Lift coefficient new Calculator

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Lift and Drag Polar

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✖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 new [C_L]

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Formula

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Lift coefficient new

Formula

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

Example

`"1.05"="10.5N"/"10Pa"`

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Lift coefficient new 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: 10.5 Newton --> 10.5 Newton No Conversion Required
Dynamic Pressure: 10 Pascal --> 10 Pascal No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

C_L = F_L/q --> 10.5/10

Evaluating ... ...

C_L = 1.05

STEP 3: Convert Result to Output's Unit

1.05 --> No Conversion Required

FINAL ANSWER

1.05 <-- Lift Coefficient

(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 coefficient new 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 new?

Lift coefficient new calculator uses Lift Coefficient = Lift Force/Dynamic Pressure to calculate the Lift Coefficient, The lift coefficient new formula is defined as the ratio of lift force action the body to the product of dynamic pressure of fluid and reference area. Lift Coefficient is denoted by C_L symbol.

How to calculate Lift coefficient new using this online calculator? To use this online calculator for Lift coefficient new, enter Lift Force (F_L) & Dynamic Pressure (q) and hit the calculate button. Here is how the Lift coefficient new calculation can be explained with given input values -> 1.05 = 10.5/10.

FAQ

What is Lift coefficient new?

The lift coefficient new formula is defined as the ratio of lift force action the body to the product of dynamic pressure of fluid and reference area 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 new?

The lift coefficient new formula is defined as the ratio of lift force action the body to the product of dynamic pressure of fluid and reference area is calculated using Lift Coefficient = Lift Force/Dynamic Pressure. To calculate Lift coefficient new, 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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