Dynamic Pressure given Coefficient of Lift Calculator

✖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 Force [F_L]			+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%
✖Area for flow decreases velocity increases and vice versa. For subsonic flows, M < 1, the behavior resembles that for incompressible flows.ⓘ Area for Flow [A]			+10% -10%

✖Dynamic Pressure is simply a convenient name for the quantity which represents the decrease in the pressure due to the velocity of the fluid.ⓘ Dynamic Pressure given Coefficient of Lift [q]

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Formula

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Dynamic Pressure given Coefficient of Lift

Formula

`"q" = "F"_{"L"}/("C"_{"L"}*"A")`

Example

`"0.190909Pa"="10.5N"/("1.1"*"50m²")`

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Dynamic Pressure given Coefficient of Lift Solution

STEP 0: Pre-Calculation Summary

Formula Used

Dynamic Pressure = Lift Force/(Lift Coefficient*Area for Flow)
q = F_L/(C_L*A)
This formula uses 4 Variables

Variables Used

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.
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.
Area for Flow - (Measured in Square Meter) - Area for flow decreases velocity increases and vice versa. For subsonic flows, M < 1, the behavior resembles that for incompressible flows.

STEP 1: Convert Input(s) to Base Unit

Lift Force: 10.5 Newton --> 10.5 Newton No Conversion Required
Lift Coefficient: 1.1 --> No Conversion Required
Area for Flow: 50 Square Meter --> 50 Square Meter No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

q = F_L/(C_L*A) --> 10.5/(1.1*50)

Evaluating ... ...

q = 0.190909090909091

STEP 3: Convert Result to Output's Unit

0.190909090909091 Pascal --> No Conversion Required

FINAL ANSWER

0.190909090909091 ≈ 0.190909 Pascal <-- Dynamic Pressure

(Calculation completed in 00.004 seconds)

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Created by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

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K J Somaiya College of Engineering (K J Somaiya), Mumbai

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< 20 Hypersonic Flow Parameters Calculators

Coefficient of Pressure with Similarity Parameters

Go Pressure Coefficient = 2*Flow Deflection angle^2*((Specific Heat Ratio+1)/4+sqrt(((Specific Heat Ratio+1)/4)^2+1/Hypersonic Similarity Parameter^2))

Pressure Ratio having High Mach Number with Similarity Constant

Go Pressure Ratio = (1-((Specific Heat Ratio-1)/2)*Hypersonic Similarity Parameter)^(2*Specific Heat Ratio/(Specific Heat Ratio-1))

Mach Number with Fluids

Go Mach Number = Fluid Velocity/(sqrt(Specific Heat Ratio*Universal Gas Constant*Final Temperature))

Pressure Ratio for High Mach Number

Go Pressure Ratio = (Mach Number ahead of shock/Mach Number behind shock)^(2*Specific Heat Ratio/(Specific Heat Ratio-1))

Moment Coefficient

Go Moment Coefficient = Moment/(Dynamic Pressure*Area for Flow*Chord Length)

Deflection Angle

Go Deflection Angle = 2/(Specific Heat Ratio-1)*(1/Mach Number ahead of shock-1/Mach Number behind shock)

Normal Force Coefficient

Go Coefficient of Force = Normal Force/(Dynamic Pressure*Area for Flow)

Supersonic Expression for Pressure Coefficient on Surface with Local Deflection Angle

Go Pressure Coefficient = (2*Deflection Angle)/(sqrt(Mach Number^2-1))

Dynamic Pressure given Coefficient of Lift

Go Dynamic Pressure = Lift Force/(Lift Coefficient*Area for Flow)

Coefficient of Drag

Go Drag Coefficient = Drag Force/(Dynamic Pressure*Area for Flow)

Dynamic Pressure

Go Dynamic Pressure = Drag Force/(Drag Coefficient*Area for Flow)

Lift Coefficient

Go Lift Coefficient = Lift Force/(Dynamic Pressure*Area for Flow)

Axial Force Coefficient

Go Coefficient of Force = Force/(Dynamic Pressure*Area for Flow)

Drag Force

Go Drag Force = Drag Coefficient*Dynamic Pressure*Area for Flow

Lift Force

Go Lift Force = Lift Coefficient*Dynamic Pressure*Area for Flow

Mach Ratio at High Mach Number

Go Mach Ratio = 1-Hypersonic Similarity Parameter*((Specific Heat Ratio-1)/2)

Hypersonic Similarity Parameter

Go Hypersonic Similarity Parameter = Mach Number*Flow Deflection angle

Shear-Stress Distribution

Go Shear Stress = Viscosity Coefficient*Velocity Gradient

Fourier's Law of Heat Conduction

Go Heat Flux = Thermal Conductivity*Temperature Gradient

Newtonian Sine Squared Law for Pressure Coefficient

Go Pressure Coefficient = 2*sin(Deflection Angle)^2

Dynamic Pressure given Coefficient of Lift Formula

Dynamic Pressure = Lift Force/(Lift Coefficient*Area for Flow)
q = F_L/(C_L*A)

What id dynamic pressure?.

In fluid dynamics, drag (sometimes called air resistance, a type of friction, or fluid resistance, another type of friction or fluid friction) is a force acting opposite to the relative motion of any object moving with respect to a surrounding fluid.[1] This can exist between two fluid layers (or surfaces) or a fluid and a solid surface

How to Calculate Dynamic Pressure given Coefficient of Lift?

Dynamic Pressure given Coefficient of Lift calculator uses Dynamic Pressure = Lift Force/(Lift Coefficient*Area for Flow) to calculate the Dynamic Pressure, The Dynamic Pressure given Coefficient of Lift formula is defined as the ratio of lift force to the product of the coefficient of lift and reference area. Dynamic Pressure is denoted by q symbol.

How to calculate Dynamic Pressure given Coefficient of Lift using this online calculator? To use this online calculator for Dynamic Pressure given Coefficient of Lift, enter Lift Force (F_L), Lift Coefficient (C_L) & Area for Flow (A) and hit the calculate button. Here is how the Dynamic Pressure given Coefficient of Lift calculation can be explained with given input values -> 0.190909 = 10.5/(1.1*50).

FAQ

What is Dynamic Pressure given Coefficient of Lift?

The Dynamic Pressure given Coefficient of Lift formula is defined as the ratio of lift force to the product of the coefficient of lift and reference area and is represented as q = F_L/(C_L*A) or Dynamic Pressure = Lift Force/(Lift Coefficient*Area for Flow). 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, 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 & Area for flow decreases velocity increases and vice versa. For subsonic flows, M < 1, the behavior resembles that for incompressible flows.

How to calculate Dynamic Pressure given Coefficient of Lift?

The Dynamic Pressure given Coefficient of Lift formula is defined as the ratio of lift force to the product of the coefficient of lift and reference area is calculated using Dynamic Pressure = Lift Force/(Lift Coefficient*Area for Flow). To calculate Dynamic Pressure given Coefficient of Lift, you need Lift Force (F_L), Lift Coefficient (C_L) & Area for Flow (A). With our tool, you need to enter the respective value for Lift Force, Lift Coefficient & Area for Flow 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 Dynamic Pressure?

In this formula, Dynamic Pressure uses Lift Force, Lift Coefficient & Area for Flow. We can use 1 other way(s) to calculate the same, which is/are as follows -

Dynamic Pressure = Drag Force/(Drag Coefficient*Area for Flow)

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