## Lift given lift coefficient Solution

STEP 0: Pre-Calculation Summary
Formula Used
Lift Force = Lift Coefficient*Dynamic Pressure
L = CL*Pdynamic
This formula uses 3 Variables
Variables Used
Lift Force - (Measured in Newton) - The lift force, lifting force or simply lift is the sum of all the forces on a body that force it to move perpendicular to the direction of 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 is simply a convenient name for the quantity which represents the decrease in the pressure due to the velocity of the 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
L = CL*Pdynamic --> 1.1*10
Evaluating ... ...
L = 11
STEP 3: Convert Result to Output's Unit
11 Newton --> No Conversion Required
11 Newton <-- Lift Force
(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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National Institute Of Technology (NIT), Hamirpur
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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

## Lift given lift coefficient Formula

Lift Force = Lift Coefficient*Dynamic Pressure
L = CL*Pdynamic

## 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 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 (CL) & Dynamic Pressure (Pdynamic) 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 L = CL*Pdynamic 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 is simply a convenient name for the quantity which represents the decrease in the pressure due to the velocity of the 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 (CL) & Dynamic Pressure (Pdynamic). 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.
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