## Lift coefficient new Solution

STEP 0: Pre-Calculation Summary
Formula Used
Lift Coefficient = Lift Force/Dynamic Pressure
CL = L/Pdynamic
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) - 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.
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 Force: 1000 Newton --> 1000 Newton No Conversion Required
Dynamic Pressure: 10 Pascal --> 10 Pascal No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
CL = L/Pdynamic --> 1000/10
Evaluating ... ...
CL = 100
STEP 3: Convert Result to Output's Unit
100 --> No Conversion Required
100 <-- Lift Coefficient
(Calculation completed in 00.000 seconds)
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## Credits

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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## < 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 coefficient new Formula

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

## 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 CL symbol.

How to calculate Lift coefficient new using this online calculator? To use this online calculator for Lift coefficient new, enter Lift Force (L) & Dynamic Pressure (Pdynamic) and hit the calculate button. Here is how the Lift coefficient new calculation can be explained with given input values -> 100 = 1000/10.

### 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 CL = L/Pdynamic or Lift Coefficient = Lift Force/Dynamic Pressure. 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 & 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 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 (L) & Dynamic Pressure (Pdynamic). 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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