Fx Copy
LaTeX Copy
Coefficient of Force is the force acting on the reference area with dynamic pressure in the case of hypersonic flow. Check FAQs
μ=FnqA
μ - Coefficient of Force?Fn - Normal Force?q - Dynamic Pressure?A - Area For Flow?

Normal Force Coefficient Example

With values
With units
Only example

Here is how the Normal Force Coefficient equation looks like with Values.

Here is how the Normal Force Coefficient equation looks like with Units.

Here is how the Normal Force Coefficient equation looks like.

0.005Edit=2.5Edit10Edit50Edit
You are here -
HomeIcon Home » Category Engineering » Category Mechanical » Category Fluid Mechanics » fx Normal Force Coefficient

Normal Force Coefficient Solution

Follow our step by step solution on how to calculate Normal Force Coefficient?

FIRST Step Consider the formula
μ=FnqA
Next Step Substitute values of Variables
μ=2.5N10Pa50
Next Step Prepare to Evaluate
μ=2.51050
LAST Step Evaluate
μ=0.005

Normal Force Coefficient Formula Elements

Variables
Coefficient of Force
Coefficient of Force is the force acting on the reference area with dynamic pressure in the case of hypersonic flow.
Symbol: μ
Measurement: NAUnit: Unitless
Note: Value should be greater than 0.
Normal Force
Normal Force is the force which is normal to the shear force.
Symbol: Fn
Measurement: ForceUnit: N
Note: Value can be positive or negative.
Dynamic Pressure
Dynamic Pressure is simply a convenient name for the quantity which represents the decrease in the pressure due to the velocity of the fluid.
Symbol: q
Measurement: PressureUnit: Pa
Note: Value should be greater than 0.
Area For Flow
Area For Flow decreases velocity increases and vice versa. For subsonic flows, M < 1, the behavior resembles that for incompressible flows.
Symbol: A
Measurement: AreaUnit:
Note: Value should be greater than 0.

Other Formulas to find Coefficient of Force

​Go Axial Force Coefficient
μ=FqA

Other formulas in Hypersonic Flow Parameters category

​Go Coefficient of Drag
CD=FDqA
​Go Coefficient of Pressure with Similarity Parameters
Cp=2θ2(Y+14+(Y+14)2+1K2)
​Go Deflection Angle
θd=2Y-1(1M1-1M2)
​Go Drag Force
FD=CDqA

How to Evaluate Normal Force Coefficient?

Normal Force Coefficient evaluator uses Coefficient of Force = Normal Force/(Dynamic Pressure*Area For Flow) to evaluate 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 evaluate Normal Force Coefficient using this online evaluator? To use this online evaluator for Normal Force Coefficient, enter Normal Force (Fn), Dynamic Pressure (q) & Area For Flow (A) and hit the calculate button.

FAQs on Normal Force Coefficient

What is the formula to find Normal Force Coefficient?
The formula of Normal Force Coefficient is expressed as Coefficient of Force = Normal Force/(Dynamic Pressure*Area For Flow). Here is an example- 0.1146 = 2.5/(10*50).
How to calculate Normal Force Coefficient?
With Normal Force (Fn), Dynamic Pressure (q) & Area For Flow (A) we can find Normal Force Coefficient using the formula - Coefficient of Force = Normal Force/(Dynamic Pressure*Area For Flow).
What are the other ways to Calculate Coefficient of Force?
Here are the different ways to Calculate Coefficient of Force-
  • Coefficient of Force=Force/(Dynamic Pressure*Area For Flow)OpenImg
Copied!