Non-Dimensional Pressure Coefficient Solution

STEP 0: Pre-Calculation Summary
Formula Used
Pressure Coefficient = Change in Static Pressure/Dynamic Pressure
Cp = Δp/Pdynamic
This formula uses 3 Variables
Variables Used
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.
Change in Static Pressure - (Measured in Pascal) - 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.
Dynamic Pressure - (Measured in Pascal) - The Dynamic Pressure is the pressure associated with the motion of a fluid, representing the kinetic energy per unit volume of the fluid flow.
STEP 1: Convert Input(s) to Base Unit
Change in Static Pressure: 5000 Pascal --> 5000 Pascal No Conversion Required
Dynamic Pressure: 11142.06 Pascal --> 11142.06 Pascal No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
Cp = Δp/Pdynamic --> 5000/11142.06
Evaluating ... ...
Cp = 0.448750051606256
STEP 3: Convert Result to Output's Unit
0.448750051606256 --> No Conversion Required
FINAL ANSWER
0.448750051606256 0.44875 <-- Pressure Coefficient
(Calculation completed in 00.004 seconds)

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Amrita School of Engineering (ASE), Vallikavu
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K J Somaiya College of Engineering (K J Somaiya), Mumbai
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Oblique Shock Relation Calculators

Parallel Upstream Flow Components after Shock as Mach Tends to Infinite
​ LaTeX ​ Go Parallel Upstream Flow Components = Velocity of the fluid at 1*(1-(2*(sin(Wave Angle))^2)/(Specific Heat Ratio-1))
Perpendicular Upstream Flow Components behind Shock Wave
​ LaTeX ​ Go Perpendicular upstream flow components = (Velocity of the fluid at 1*sin(2*Wave Angle))/(Specific Heat Ratio-1)
Wave Angle for Small Deflection Angle
​ LaTeX ​ Go Wave Angle = (Specific Heat Ratio+1)/2*(Deflection Angle*180/pi)*pi/180
Coefficient of Pressure Derived from Oblique Shock Theory
​ LaTeX ​ Go Pressure Coefficient = 2*(sin(Wave Angle))^2

Non-Dimensional Pressure Coefficient Formula

​LaTeX ​Go
Pressure Coefficient = Change in Static Pressure/Dynamic Pressure
Cp = Δp/Pdynamic

What is the pressure coefficient of oblique shock?

The pressure coefficient is a dimensionless number which describes the relative pressures throughout a flow field in fluid dynamics. The pressure coefficient is used in aerodynamics and hydrodynamics.

How to Calculate Non-Dimensional Pressure Coefficient?

Non-Dimensional Pressure Coefficient calculator uses Pressure Coefficient = Change in Static Pressure/Dynamic Pressure to calculate 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 calculate Non-Dimensional Pressure Coefficient using this online calculator? To use this online calculator for Non-Dimensional Pressure Coefficient, enter Change in Static Pressure (Δp) & Dynamic Pressure (Pdynamic) and hit the calculate button. Here is how the Non-Dimensional Pressure Coefficient calculation can be explained with given input values -> 0.44875 = 5000/11142.06.

FAQ

What is Non-Dimensional 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 and is represented as Cp = Δp/Pdynamic or Pressure Coefficient = Change in Static Pressure/Dynamic 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 & The Dynamic Pressure is the pressure associated with the motion of a fluid, representing the kinetic energy per unit volume of the fluid flow.
How to calculate Non-Dimensional 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 is calculated using Pressure Coefficient = Change in Static Pressure/Dynamic Pressure. To calculate Non-Dimensional Pressure Coefficient, you need Change in Static Pressure (Δp) & Dynamic Pressure (Pdynamic). With our tool, you need to enter the respective value for Change in Static Pressure & Dynamic Pressure 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 Pressure Coefficient?
In this formula, Pressure Coefficient uses Change in Static Pressure & Dynamic Pressure. We can use 3 other way(s) to calculate the same, which is/are as follows -
  • Pressure Coefficient = 2*(sin(Wave Angle))^2
  • Pressure Coefficient = 4/(Specific Heat Ratio+1)*((sin(Wave Angle))^2-1/Mach Number^2)
  • Pressure Coefficient = 4/(Specific Heat Ratio+1)*(sin(Wave Angle))^2
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