Drag given lift coefficient Calculator

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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%
✖Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water.ⓘ Drag Coefficient [C_D]			+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 [C_L]			+10% -10%

✖Drag Force is the resisting force experienced by an object moving through a fluid ,such as air.ⓘ Drag given lift coefficient [F_D]

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Drag given lift coefficient

Formula

`"F"_{"D"} = "F"_{"L"}*"C"_{"D"}/"C"_{"L"}`

Example

`"286.3636N"="10.5N"*"30"/"1.1"`

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Drag given lift coefficient Solution

STEP 0: Pre-Calculation Summary

Formula Used

Drag Force = Lift Force*Drag Coefficient/Lift Coefficient
F_D = F_L*C_D/C_L
This formula uses 4 Variables

Variables Used

Drag Force - (Measured in Newton) - Drag Force is the resisting force experienced by an object moving through a fluid ,such as air.
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.
Drag Coefficient - Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water.
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.

STEP 1: Convert Input(s) to Base Unit

Lift Force: 10.5 Newton --> 10.5 Newton No Conversion Required
Drag Coefficient: 30 --> No Conversion Required
Lift Coefficient: 1.1 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

F_D = F_L*C_D/C_L --> 10.5*30/1.1

Evaluating ... ...

F_D = 286.363636363636

STEP 3: Convert Result to Output's Unit

286.363636363636 Newton --> No Conversion Required

FINAL ANSWER

286.363636363636 ≈ 286.3636 Newton <-- Drag Force

(Calculation completed in 00.004 seconds)

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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

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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

Drag given lift coefficient Formula

Drag Force = Lift Force*Drag Coefficient/Lift Coefficient
F_D = F_L*C_D/C_L

What is drag?

In fluid dynamics, drag is a force acting opposite to the relative motion of any object moving with respect to a surrounding fluid.

How to Calculate Drag given lift coefficient?

Drag given lift coefficient calculator uses Drag Force = Lift Force*Drag Coefficient/Lift Coefficient to calculate the Drag Force, The Drag given lift coefficient formula is defined as a way to find aerodynamic efficiency of the object travelling under lift and drag forces. Drag Force is denoted by F_D symbol.

How to calculate Drag given lift coefficient using this online calculator? To use this online calculator for Drag given lift coefficient, enter Lift Force (F_L), Drag Coefficient (C_D) & Lift Coefficient (C_L) and hit the calculate button. Here is how the Drag given lift coefficient calculation can be explained with given input values -> 286.3636 = 10.5*30/1.1.

FAQ

What is Drag given lift coefficient?

The Drag given lift coefficient formula is defined as a way to find aerodynamic efficiency of the object travelling under lift and drag forces and is represented as F_D = F_L*C_D/C_L or Drag Force = Lift Force*Drag Coefficient/Lift Coefficient. Lift force is the component of the total force acting on a body that is perpendicular to the direction of the fluid flow, Drag Coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water & 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.

How to calculate Drag given lift coefficient?

The Drag given lift coefficient formula is defined as a way to find aerodynamic efficiency of the object travelling under lift and drag forces is calculated using Drag Force = Lift Force*Drag Coefficient/Lift Coefficient. To calculate Drag given lift coefficient, you need Lift Force (F_L), Drag Coefficient (C_D) & Lift Coefficient (C_L). With our tool, you need to enter the respective value for Lift Force, Drag Coefficient & Lift Coefficient 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 Drag Force?

In this formula, Drag Force uses Lift Force, Drag Coefficient & Lift Coefficient. We can use 3 other way(s) to calculate the same, which is/are as follows -

Drag Force = Drag Coefficient*Dynamic Pressure
Drag Force = Gross Weight/Lift Coefficient/Drag Coefficient
Drag Force = Aerodynamic Force-Lift Force

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