Normal Force Coefficient Solution

STEP 0: Pre-Calculation Summary
Formula Used
Coefficient of Force = Normal Force/(Dynamic Pressure*Area for Flow)
μ = Fn/(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: 57.3 Newton --> 57.3 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 = Fn/(q*A) --> 57.3/(10*50)
Evaluating ... ...
μ = 0.1146
STEP 3: Convert Result to Output's Unit
0.1146 --> No Conversion Required
FINAL ANSWER
0.1146 <-- Coefficient of Force
(Calculation completed in 00.004 seconds)

Credits

Created by Sanjay Krishna
Amrita School of Engineering (ASE), Vallikavu
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Verified by Vinay Mishra
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

Normal Force Coefficient Formula

Coefficient of Force = Normal Force/(Dynamic Pressure*Area for Flow)
μ = Fn/(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, The Normal Force Coefficient is defined as the ratio of force acting normally to the body in hypersonic flow to the product of dynamic pressure and area. 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 (Fn), 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 = 57.3/(10*50).

FAQ

What is Normal Force Coefficient?
The Normal Force Coefficient is defined as the ratio of force acting normally to the body in hypersonic flow to the product of dynamic pressure and area and is represented as μ = Fn/(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?
The Normal Force Coefficient is defined as the ratio of force acting normally to the body in hypersonic flow to the product of dynamic pressure and area is calculated using Coefficient of Force = Normal Force/(Dynamic Pressure*Area for Flow). To calculate Normal Force Coefficient, you need Normal Force (Fn), 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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