Axial Force Coefficient Calculator

✖Force on Fluid Element is the sum of pressure and shear forces acting on it within a fluid system.ⓘ Force [F]			+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 [q]			+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%

✖Coefficient of Force is the force acting on the reference area with dynamic pressure in the case of hypersonic flow.ⓘ Axial Force Coefficient [μ]

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Formula

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Axial Force Coefficient

Formula

`"μ" = "F"/("q"*"A")`

Example

`"0.005"="2.5N"/("10Pa"*"50m²")`

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Axial Force Coefficient Solution

STEP 0: Pre-Calculation Summary

Formula Used

Coefficient of Force = Force/(Dynamic Pressure*Area for Flow)
μ = F/(q*A)
This formula uses 4 Variables

Variables Used

Coefficient of Force - Coefficient of Force is the force acting on the reference area with dynamic pressure in the case of hypersonic flow.
Force - (Measured in Newton) - Force on Fluid Element is the sum of pressure and shear forces acting on it within a fluid system.
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.
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

Force: 2.5 Newton --> 2.5 Newton No Conversion Required
Dynamic Pressure: 10 Pascal --> 10 Pascal No Conversion Required
Area for Flow: 50 Square Meter --> 50 Square Meter No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

μ = F/(q*A) --> 2.5/(10*50)

Evaluating ... ...

μ = 0.005

STEP 3: Convert Result to Output's Unit

0.005 --> No Conversion Required

FINAL ANSWER

0.005 <-- Coefficient of Force

(Calculation completed in 00.020 seconds)

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Created by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

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Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune

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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

Axial Force Coefficient Formula

Coefficient of Force = Force/(Dynamic Pressure*Area for Flow)
μ = F/(q*A)

What is axial Force coefficient?

Axial force coefficient is mainly used o calculate the axial force acting on the body moving at a hypersonic velocity in the fluid.

How to Calculate Axial Force Coefficient?

Axial Force Coefficient calculator uses Coefficient of Force = Force/(Dynamic Pressure*Area for Flow) to calculate the Coefficient of Force, The Axial force coefficient formula is defined as the ratio of force acting axially to the product of dynamic pressure and area, for compressible flow. Coefficient of Force is denoted by μ symbol.

How to calculate Axial Force Coefficient using this online calculator? To use this online calculator for Axial Force Coefficient, enter Force (F), Dynamic Pressure (q) & Area for Flow (A) and hit the calculate button. Here is how the Axial Force Coefficient calculation can be explained with given input values -> 0.005 = 2.5/(10*50).

FAQ

What is Axial Force Coefficient?

The Axial force coefficient formula is defined as the ratio of force acting axially to the product of dynamic pressure and area, for compressible flow and is represented as μ = F/(q*A) or Coefficient of Force = Force/(Dynamic Pressure*Area for Flow). Force on Fluid Element is the sum of pressure and shear forces acting on it within a fluid system, Dynamic Pressure is simply a convenient name for the quantity which represents the decrease in the pressure due to the velocity of the fluid & Area for flow decreases velocity increases and vice versa. For subsonic flows, M < 1, the behavior resembles that for incompressible flows.

How to calculate Axial Force Coefficient?

The Axial force coefficient formula is defined as the ratio of force acting axially to the product of dynamic pressure and area, for compressible flow is calculated using Coefficient of Force = Force/(Dynamic Pressure*Area for Flow). To calculate Axial Force Coefficient, you need Force (F), Dynamic Pressure (q) & Area for Flow (A). With our tool, you need to enter the respective value for Force, Dynamic Pressure & 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 Coefficient of Force?

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

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

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