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The Pressure Coefficient is a dimensionless number that represents the relative pressure difference across a surface in fluid flow, indicating how pressure varies in different flow conditions. Check FAQs
Cp=ΔpPdynamic
Cp - Pressure Coefficient?Δp - Change in Static Pressure?Pdynamic - Dynamic Pressure?

Non-Dimensional Pressure Coefficient Example

With values
With units
Only example

Here is how the Non-Dimensional Pressure Coefficient equation looks like with Values.

Here is how the Non-Dimensional Pressure Coefficient equation looks like with Units.

Here is how the Non-Dimensional Pressure Coefficient equation looks like.

0.4488Edit=5000Edit11142.06Edit
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Non-Dimensional Pressure Coefficient Solution

Follow our step by step solution on how to calculate Non-Dimensional Pressure Coefficient?

FIRST Step Consider the formula
Cp=ΔpPdynamic
Next Step Substitute values of Variables
Cp=5000Pa11142.06Pa
Next Step Prepare to Evaluate
Cp=500011142.06
Next Step Evaluate
Cp=0.448750051606256
LAST Step Rounding Answer
Cp=0.4488

Non-Dimensional Pressure Coefficient Formula Elements

Variables
Pressure Coefficient
The Pressure Coefficient is a dimensionless number that represents the relative pressure difference across a surface in fluid flow, indicating how pressure varies in different flow conditions.
Symbol: Cp
Measurement: NAUnit: Unitless
Note: Value can be positive or negative.
Change in Static Pressure
The Change in Static Pressure is the difference in pressure experienced by a fluid as it flows through a system, influencing its behavior and performance in various applications.
Symbol: Δp
Measurement: PressureUnit: Pa
Note: Value should be greater than 0.
Dynamic Pressure
The Dynamic Pressure is the pressure associated with the motion of a fluid, representing the kinetic energy per unit volume of the fluid flow.
Symbol: Pdynamic
Measurement: PressureUnit: Pa
Note: Value should be greater than 0.

Other Formulas to find Pressure Coefficient

​Go Coefficient of Pressure Derived from Oblique Shock Theory
Cp=2(sin(β))2
​Go Pressure Coefficient behind Oblique Shock Wave
Cp=4Y+1((sin(β))2-1M2)
​Go Pressure Coefficient behind Oblique Shock Wave for Infinite Mach Number
Cp=4Y+1(sin(β))2

Other formulas in Oblique Shock Relation category

​Go Wave Angle for Small Deflection Angle
β=Y+12(θd180π)π180
​Go Parallel Upstream Flow Components after Shock as Mach Tends to Infinite
u2=V1(1-2(sin(β))2Y-1)
​Go Perpendicular Upstream Flow Components behind Shock Wave
v2=V1(sin(2β))Y-1
​Go Exact Pressure Ratio
rp=1+2YY+1((Msin(β))2-1)

How to Evaluate Non-Dimensional Pressure Coefficient?

Non-Dimensional Pressure Coefficient evaluator uses Pressure Coefficient = Change in Static Pressure/Dynamic Pressure to evaluate the Pressure Coefficient, Non-Dimensional Pressure Coefficient formula is defined as a dimensionless quantity that characterizes the pressure ratio across an oblique shock wave, providing a crucial parameter in understanding the behavior of compressible flows and shock waves in various engineering applications. Pressure Coefficient is denoted by Cp symbol.

How to evaluate Non-Dimensional Pressure Coefficient using this online evaluator? To use this online evaluator for Non-Dimensional Pressure Coefficient, enter Change in Static Pressure (Δp) & Dynamic Pressure (Pdynamic) and hit the calculate button.

FAQs on Non-Dimensional Pressure Coefficient

What is the formula to find Non-Dimensional Pressure Coefficient?
The formula of Non-Dimensional Pressure Coefficient is expressed as Pressure Coefficient = Change in Static Pressure/Dynamic Pressure. Here is an example- 0.44875 = 5000/11142.06.
How to calculate Non-Dimensional Pressure Coefficient?
With Change in Static Pressure (Δp) & Dynamic Pressure (Pdynamic) we can find Non-Dimensional Pressure Coefficient using the formula - Pressure Coefficient = Change in Static Pressure/Dynamic Pressure.
What are the other ways to Calculate Pressure Coefficient?
Here are the different ways to Calculate Pressure Coefficient-
  • Pressure Coefficient=2*(sin(Wave Angle))^2OpenImg
  • Pressure Coefficient=4/(Specific Heat Ratio+1)*((sin(Wave Angle))^2-1/Mach Number^2)OpenImg
  • Pressure Coefficient=4/(Specific Heat Ratio+1)*(sin(Wave Angle))^2OpenImg
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