Stagnation Pressure considering other Stagnation Properties of Fluid Calculator

✖Stagnation Temperature in Compressible Flow is defined as the temperature of the fluid at a stagnation point in the compressible fluid flow.ⓘ Stagnation Temperature in Compressible Flow [T_s]			+10% -10%
✖Gas Constant in Compressible Flow is a physical constant that appears in an equation defining the behavior of a gas under theoretically ideal conditions.ⓘ Gas Constant in Compressible Flow [R]			+10% -10%
✖Stagnation Density in Compressible Flow is defined as the density of the fluid at a stagnation point in the compressible fluid flow.ⓘ Stagnation Density in Compressible Flow [ρ_s]			+10% -10%

✖Stagnation Pressure in Compressible Flow is defined as the pressure of the fluid at a stagnation point in the compressible fluid flow.ⓘ Stagnation Pressure considering other Stagnation Properties of Fluid [p_s]

⎘ Copy

👎

Formula

LaTeX

Reset

👍

Download Fluid Mechanics Formula PDF PDF Image

Stagnation Pressure considering other Stagnation Properties of Fluid Solution

STEP 0: Pre-Calculation Summary

Formula Used

Stagnation Pressure in Compressible Flow = Stagnation Temperature in Compressible Flow*Gas Constant in Compressible Flow*Stagnation Density in Compressible Flow
p_s = T_s*R*ρ_s
This formula uses 4 Variables

Variables Used

Stagnation Pressure in Compressible Flow - (Measured in Pascal) - Stagnation Pressure in Compressible Flow is defined as the pressure of the fluid at a stagnation point in the compressible fluid flow.
Stagnation Temperature in Compressible Flow - (Measured in Kelvin) - Stagnation Temperature in Compressible Flow is defined as the temperature of the fluid at a stagnation point in the compressible fluid flow.
Gas Constant in Compressible Flow - (Measured in Joule per Kilogram per K) - Gas Constant in Compressible Flow is a physical constant that appears in an equation defining the behavior of a gas under theoretically ideal conditions.
Stagnation Density in Compressible Flow - (Measured in Kilogram per Cubic Meter) - Stagnation Density in Compressible Flow is defined as the density of the fluid at a stagnation point in the compressible fluid flow.

STEP 1: Convert Input(s) to Base Unit

Stagnation Temperature in Compressible Flow: 314 Kelvin --> 314 Kelvin No Conversion Required
Gas Constant in Compressible Flow: 287.14 Joule per Kilogram per K --> 287.14 Joule per Kilogram per K No Conversion Required
Stagnation Density in Compressible Flow: 2.5218 Kilogram per Cubic Meter --> 2.5218 Kilogram per Cubic Meter No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

p_s = T_s*R*ρ_s --> 314*287.14*2.5218

Evaluating ... ...

p_s = 227370.430728

STEP 3: Convert Result to Output's Unit

227370.430728 Pascal -->227370.430728 Newton per Square Meter (Check conversion here)

FINAL ANSWER

227370.430728 ≈ 227370.4 Newton per Square Meter <-- Stagnation Pressure in Compressible Flow

(Calculation completed in 00.004 seconds)

You are here -

Home » Physics » Fluid Mechanics » Flow Characteristics » Compressible Flow » Mechanical » Stagnation Properties » Stagnation Pressure considering other Stagnation Properties of Fluid

Credits

Created by Maiarutselvan V

PSG College of Technology (PSGCT), Coimbatore

Maiarutselvan V has created this Calculator and 300+ more calculators!

Verified by Sai Venkata Phanindra Chary Arendra

Vallurupalli Nageswara Rao Vignana Jyothi Institute of Engineering and Technology (VNRVJIET), Hyderabad

Sai Venkata Phanindra Chary Arendra has verified this Calculator and 300+ more calculators!

< Stagnation Properties Calculators

Stagnation Pressure for Compressible Fluid Flow

LaTeX Go Stagnation Pressure in Compressible Flow = Pressure of Still Air*(1+(Specific Heat Ratio-1)/2*Mach Number For Compressible Flow^2)^(Specific Heat Ratio/(Specific Heat Ratio-1))

Density of Fluid for Stagnation considering Compressible Fluid Flow

LaTeX Go Density of Air Medium = Stagnation Density in Compressible Flow/(1+(Specific Heat Ratio-1)/2*Mach Number For Compressible Flow^2)^(1/(Specific Heat Ratio-1))

Stagnation Density given Compressible Fluid Flow

LaTeX Go Stagnation Density in Compressible Flow = Density of Air Medium*(1+(Specific Heat Ratio-1)/2*Mach Number For Compressible Flow^2)^(1/(Specific Heat Ratio-1))

Stagnation Density considering other Stagnation Properties of Fluid

LaTeX Go Stagnation Density in Compressible Flow = Stagnation Pressure in Compressible Flow/(Gas Constant in Compressible Flow*Stagnation Temperature in Compressible Flow)

Stagnation Pressure considering other Stagnation Properties of Fluid Formula

LaTeX Go

Stagnation Pressure in Compressible Flow = Stagnation Temperature in Compressible Flow*Gas Constant in Compressible Flow*Stagnation Density in Compressible Flow
p_s = T_s*R*ρ_s

What is the stagnation properties of fluid?

When a fluid flows past an immersed body if the resultant velocity of the fluid at a point on the body becomes zero, the values of pressure, temperature, and density at that point will be termed as stagnation properties.

What is a stagnation point in fluid mechanics?

In fluid dynamics, a stagnation point is a point in a flow field where the local velocity of the fluid is zero. Stagnation points exist at the surface of objects in the flow field, where the fluid is brought to rest by the object.

How to Calculate Stagnation Pressure considering other Stagnation Properties of Fluid?

Stagnation Pressure considering other Stagnation Properties of Fluid calculator uses Stagnation Pressure in Compressible Flow = Stagnation Temperature in Compressible Flow*Gas Constant in Compressible Flow*Stagnation Density in Compressible Flow to calculate the Stagnation Pressure in Compressible Flow, Stagnation Pressure considering other Stagnation Properties of Fluid , refers to the pressure of the fluid when it comes to rest under stagnation conditions. This pressure is influenced by factors such as stagnation density, temperature, and velocity, and understanding it is essential in aerodynamics, thermodynamics, and fluid dynamics for accurately predicting fluid behavior in various applications, including aircraft design, engine performance, and gas dynamics. Stagnation Pressure in Compressible Flow is denoted by p_s symbol.

How to calculate Stagnation Pressure considering other Stagnation Properties of Fluid using this online calculator? To use this online calculator for Stagnation Pressure considering other Stagnation Properties of Fluid, enter Stagnation Temperature in Compressible Flow (T_s), Gas Constant in Compressible Flow (R) & Stagnation Density in Compressible Flow (ρ_s) and hit the calculate button. Here is how the Stagnation Pressure considering other Stagnation Properties of Fluid calculation can be explained with given input values -> 227370.4 = 314*287.14*2.5218.

FAQ

What is Stagnation Pressure considering other Stagnation Properties of Fluid?

Stagnation Pressure considering other Stagnation Properties of Fluid , refers to the pressure of the fluid when it comes to rest under stagnation conditions. This pressure is influenced by factors such as stagnation density, temperature, and velocity, and understanding it is essential in aerodynamics, thermodynamics, and fluid dynamics for accurately predicting fluid behavior in various applications, including aircraft design, engine performance, and gas dynamics and is represented as p_s = T_s*R*ρ_s or Stagnation Pressure in Compressible Flow = Stagnation Temperature in Compressible Flow*Gas Constant in Compressible Flow*Stagnation Density in Compressible Flow. Stagnation Temperature in Compressible Flow is defined as the temperature of the fluid at a stagnation point in the compressible fluid flow, Gas Constant in Compressible Flow is a physical constant that appears in an equation defining the behavior of a gas under theoretically ideal conditions & Stagnation Density in Compressible Flow is defined as the density of the fluid at a stagnation point in the compressible fluid flow.

How to calculate Stagnation Pressure considering other Stagnation Properties of Fluid?

Stagnation Pressure considering other Stagnation Properties of Fluid , refers to the pressure of the fluid when it comes to rest under stagnation conditions. This pressure is influenced by factors such as stagnation density, temperature, and velocity, and understanding it is essential in aerodynamics, thermodynamics, and fluid dynamics for accurately predicting fluid behavior in various applications, including aircraft design, engine performance, and gas dynamics is calculated using Stagnation Pressure in Compressible Flow = Stagnation Temperature in Compressible Flow*Gas Constant in Compressible Flow*Stagnation Density in Compressible Flow. To calculate Stagnation Pressure considering other Stagnation Properties of Fluid, you need Stagnation Temperature in Compressible Flow (T_s), Gas Constant in Compressible Flow (R) & Stagnation Density in Compressible Flow (ρ_s). With our tool, you need to enter the respective value for Stagnation Temperature in Compressible Flow, Gas Constant in Compressible Flow & Stagnation Density in Compressible 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 Stagnation Pressure in Compressible Flow?

In this formula, Stagnation Pressure in Compressible Flow uses Stagnation Temperature in Compressible Flow, Gas Constant in Compressible Flow & Stagnation Density in Compressible Flow. We can use 1 other way(s) to calculate the same, which is/are as follows -

Stagnation Pressure in Compressible Flow = Pressure of Still Air*(1+(Specific Heat Ratio-1)/2*Mach Number For Compressible Flow^2)^(Specific Heat Ratio/(Specific Heat Ratio-1))

Home

FREE PDFs

🔍 Search