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Pressure coefficient defines the value of local pressure at a point in terms of free stream pressure and dynamic pressure. 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.

0.5814Edit=5Edit8.6Edit
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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=5Pa8.6Pa
Next Step Prepare to Evaluate
Cp=58.6
Next Step Evaluate
Cp=0.581395348837209
LAST Step Rounding Answer
Cp=0.5814

Non-Dimensional Pressure Coefficient Formula Elements

Variables
Pressure Coefficient
Pressure coefficient defines the value of local pressure at a point in terms of free stream pressure and dynamic pressure.
Symbol: Cp
Measurement: NAUnit: Unitless
Note: Value can be positive or negative.
Change in Static Pressure
Change in static pressure is the static pressure change occurring in hypersonic flow after shock occurs.
Symbol: Δp
Measurement: PressureUnit: Pa
Note: Value should be greater than 0.
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: 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- 0.581395 = 5/8.6.
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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