Normal Force Coefficient Calculator

✖Normal Force is the force which is normal to the shear force.ⓘ Normal Force [F_n]			+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.ⓘ Normal Force Coefficient [μ]

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Normal Force Coefficient Solution

STEP 0: Pre-Calculation Summary

Formula Used

Coefficient of Force = Normal Force/(Dynamic Pressure*Area For Flow)
μ = F_n/(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.
Normal Force - (Measured in Newton) - Normal Force is the force which is normal to the shear force.
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

Normal 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_n/(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 00.004 seconds)

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Created by Sanjay Krishna

Amrita School of Engineering (ASE), Vallikavu

Sanjay Krishna has created this Calculator and 300+ more calculators!

Verified by Vinay Mishra

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

Vinay Mishra has verified this Calculator and 100+ more calculators!

< Hypersonic Flow Parameters Calculators

Coefficient of Pressure with Similarity Parameters

LaTeX 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))

Deflection Angle

LaTeX Go Deflection Angle = 2/(Specific Heat Ratio-1)*(1/Mach Number ahead of Shock-1/Mach Number Behind Shock)

Coefficient of Drag

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

Axial Force Coefficient

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

Normal Force Coefficient Formula

LaTeX Go

Coefficient of Force = Normal Force/(Dynamic Pressure*Area For Flow)
μ = F_n/(q*A)

What is Normal Force Coefficient?

It is the coefficient of force acting on the body due to the compressible flow or flows having hypersonic velocities.

How to Calculate Normal Force Coefficient?

Normal Force Coefficient calculator uses Coefficient of Force = Normal Force/(Dynamic Pressure*Area For Flow) to calculate the Coefficient of Force, Normal Force Coefficient formula is defined as a dimensionless quantity that characterizes the normal force experienced by a body in hypersonic flow, providing a crucial parameter in the analysis of high-speed flight and re-entry vehicles, where the interaction between the vehicle and the surrounding air is critical. Coefficient of Force is denoted by μ symbol.

How to calculate Normal Force Coefficient using this online calculator? To use this online calculator for Normal Force Coefficient, enter Normal Force (F_n), Dynamic Pressure (q) & Area For Flow (A) and hit the calculate button. Here is how the Normal Force Coefficient calculation can be explained with given input values -> 0.1146 = 2.5/(10*50).

FAQ

What is Normal Force Coefficient?

Normal Force Coefficient formula is defined as a dimensionless quantity that characterizes the normal force experienced by a body in hypersonic flow, providing a crucial parameter in the analysis of high-speed flight and re-entry vehicles, where the interaction between the vehicle and the surrounding air is critical and is represented as μ = F_n/(q*A) or Coefficient of Force = Normal Force/(Dynamic Pressure*Area For Flow). Normal Force is the force which is normal to the shear force, 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 Normal Force Coefficient?

Normal Force Coefficient formula is defined as a dimensionless quantity that characterizes the normal force experienced by a body in hypersonic flow, providing a crucial parameter in the analysis of high-speed flight and re-entry vehicles, where the interaction between the vehicle and the surrounding air is critical is calculated using Coefficient of Force = Normal Force/(Dynamic Pressure*Area For Flow). To calculate Normal Force Coefficient, you need Normal Force (F_n), Dynamic Pressure (q) & Area For Flow (A). With our tool, you need to enter the respective value for Normal 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 Normal 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 = Force/(Dynamic Pressure*Area For Flow)

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