## Coefficient of drag given drag Solution

STEP 0: Pre-Calculation Summary
Formula Used
Drag Coefficient = (Lift Coefficient*Drag Force)/Gross Weight
CD = (CL*FD)/W0
This formula uses 4 Variables
Variables Used
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.
Drag Force - (Measured in Newton) - Drag Force is the resisting force experienced by an object moving through a fluid.
Gross Weight - (Measured in Kilogram) - The Gross Weight of the airplane is the weight with full fuel and payload.
STEP 1: Convert Input(s) to Base Unit
Lift Coefficient: 1.1 --> No Conversion Required
Drag Force: 80 Newton --> 80 Newton No Conversion Required
Gross Weight: 5000 Kilogram --> 5000 Kilogram No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
CD = (CL*FD)/W0 --> (1.1*80)/5000
Evaluating ... ...
CD = 0.0176
STEP 3: Convert Result to Output's Unit
0.0176 --> No Conversion Required
0.0176 <-- Drag Coefficient
(Calculation completed in 00.016 seconds)
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## Credits

Created by Himanshu Sharma
National Institute of Technology, Hamirpur (NITH), Himachal Pradesh
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## < 10+ Aerodynamic Drag and Its Reduction Calculators

Coefficient of lift given drag

## Coefficient of lift given drag

Formula
"C"_{"L"} = ("W"_{"0"}*"C"_{"D"})/"F"_{"D"}

Example
"1875"=("5000kg"*"30")/"80N"

Calculator
LaTeX
Lift Coefficient = (Gross Weight*Drag Coefficient)/Drag Force
Coefficient of drag given drag

## Coefficient of drag given drag

Formula
"C"_{"D"} = ("C"_{"L"}*"F"_{"D"})/"W"_{"0"}

Example
"0.0176"=("1.1"*"80N")/"5000kg"

Calculator
LaTeX
Drag Coefficient = (Lift Coefficient*Drag Force)/Gross Weight
Gross weight given drag

## Gross weight given drag

Formula
"W"_{"0"} = "F"_{"D"}*("C"_{"L"}/"C"_{"D"})

Example
"2.933333kg"="80N"*("1.1"/"30")

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

## Drag

Formula
"F"_{"D"} = "W"_{"0"}/"C"_{"L"}/"C"_{"D"}

Example
"151.5152N"="5000kg"/"1.1"/"30"

Calculator
LaTeX
Drag Force = Gross Weight/Lift Coefficient/Drag Coefficient
Ambient air density given dynamic pressure

## Ambient air density given dynamic pressure

Formula
"ρ" = 2*"P"_{"dynamic"}/("V"^2)

Example
"0.005767kg/m³"=2*"10Pa"/("212km/h"^2)

Calculator
LaTeX
Ambient air density = 2*Dynamic Pressure/(Flight speed^2)
Flight speed given dynamic pressure

## Flight speed given dynamic pressure

Formula
"V" = 2*"P"_{"dynamic"}/("ρ")

Example
"58.77551km/h"=2*"10Pa"/("1.225kg/m³")

Calculator
LaTeX
Flight speed = 2*Dynamic Pressure/(Ambient air density)
Lift given lift coefficient

## Lift given lift coefficient

Formula
"L" = "C"_{"L"}*"P"_{"dynamic"}

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

Calculator
LaTeX
Lift Force = Lift Coefficient*Dynamic Pressure
Drag given drag coefficient

## Drag given drag coefficient

Formula
"F"_{"D"} = "C"_{"D"}*"P"_{"dynamic"}

Example
"300N"="30"*"10Pa"

Calculator
LaTeX
Drag Force = Drag Coefficient*Dynamic Pressure
Lift coefficient new

## Lift coefficient new

Formula
"C"_{"L"} = "L"/"P"_{"dynamic"}

Example
"100"="1000N"/"10Pa"

Calculator
LaTeX
Lift Coefficient = Lift Force/Dynamic Pressure
Drag coefficient new

## Drag coefficient new

Formula
"C"_{"D"} = "F"_{"D"}/"P"_{"dynamic"}

Example
"8"="80N"/"10Pa"

Calculator
LaTeX
Drag Coefficient = Drag Force/Dynamic Pressure

## Coefficient of drag given drag Formula

Drag Coefficient = (Lift Coefficient*Drag Force)/Gross Weight
CD = (CL*FD)/W0

## What is drag coefficient?

In fluid dynamics, the 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. It is used in the drag equation in which a lower drag coefficient indicates the object will have less aerodynamic or hydrodynamic drag.

## How to Calculate Coefficient of drag given drag?

Coefficient of drag given drag calculator uses Drag Coefficient = (Lift Coefficient*Drag Force)/Gross Weight to calculate the Drag Coefficient, The Coefficient of drag given drag formula is defined as drag experianced by the aircraft during its flight by the air considering gross weight, drag force and generated lift. Drag Coefficient is denoted by CD symbol.

How to calculate Coefficient of drag given drag using this online calculator? To use this online calculator for Coefficient of drag given drag, enter Lift Coefficient (CL), Drag Force (FD) & Gross Weight (W0) and hit the calculate button. Here is how the Coefficient of drag given drag calculation can be explained with given input values -> 0.0176 = (1.1*80)/5000.

### FAQ

What is Coefficient of drag given drag?
The Coefficient of drag given drag formula is defined as drag experianced by the aircraft during its flight by the air considering gross weight, drag force and generated lift and is represented as CD = (CL*FD)/W0 or Drag Coefficient = (Lift Coefficient*Drag Force)/Gross Weight. 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, Drag Force is the resisting force experienced by an object moving through a fluid & The Gross Weight of the airplane is the weight with full fuel and payload.
How to calculate Coefficient of drag given drag?
The Coefficient of drag given drag formula is defined as drag experianced by the aircraft during its flight by the air considering gross weight, drag force and generated lift is calculated using Drag Coefficient = (Lift Coefficient*Drag Force)/Gross Weight. To calculate Coefficient of drag given drag, you need Lift Coefficient (CL), Drag Force (FD) & Gross Weight (W0). With our tool, you need to enter the respective value for Lift Coefficient, Drag Force & Gross Weight 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 Coefficient?
In this formula, Drag Coefficient uses Lift Coefficient, Drag Force & Gross Weight. We can use 2 other way(s) to calculate the same, which is/are as follows -
• Drag Coefficient = Drag Force/Dynamic Pressure
• Drag Coefficient = Lift Coefficient*Drag Force/Lift Force Let Others Know