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
FINAL ANSWER
100 <-- Lift Coefficient
(Calculation completed in 00.000 seconds)

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
Kartikay Pandit has verified this Calculator and 200+ more calculators!

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
Go 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
Go 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
Go 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
Go 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
Go 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
Go 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
Go 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
Go Drag Force = Drag Coefficient*Dynamic Pressure
Lift coefficient new

Lift coefficient new

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

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

Calculator
LaTeX
Go 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
Go 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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