Stagnation Temperature considering other Stagnation Properties of Fluid Calculator

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Stagnation Properties

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

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Formula

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Stagnation Temperature considering other Stagnation Properties of Fluid

Formula

`"T"_{"s"} = "p"_{"s"}/("R"*"ρ"_{"s"})`

Example

`"168.6031K"="1.22E5N/m²"/("287.14J/(kg*K)"*"2.52kg/m³")`

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Stagnation Temperature considering other Stagnation Properties of Fluid Solution

STEP 0: Pre-Calculation Summary

Formula Used

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

Variables Used

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.
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.
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 Pressure in Compressible Flow: 122000 Newton per Square Meter --> 122000 Pascal (Check conversion here)
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: 2.52 Kilogram per Cubic Meter --> 2.52 Kilogram per Cubic Meter No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

T_s = p_s/(R*ρ_s) --> 122000/(287.14*2.52)

Evaluating ... ...

T_s = 168.603114901088

STEP 3: Convert Result to Output's Unit

168.603114901088 Kelvin --> No Conversion Required

FINAL ANSWER

168.603114901088 ≈ 168.6031 Kelvin <-- Stagnation Temperature in Compressible Flow

(Calculation completed in 00.020 seconds)

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< 8 Stagnation Properties Calculators

Stagnation Pressure for Compressible Fluid Flow

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

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

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 Temperature considering other Stagnation Properties of Fluid

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

Stagnation Density considering other Stagnation Properties of Fluid

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

Go Stagnation Pressure in Compressible Flow = Stagnation Temperature in Compressible Flow*Gas Constant in Compressible Flow*Stagnation Density in Compressible Flow

Temperature of Fluid for Stagnation Temperature considering Compressible Fluid Flow

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

Stagnation Temperature considering Compressible Fluid Flow

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

Stagnation Temperature considering other Stagnation Properties of Fluid Formula

Stagnation Temperature in Compressible Flow = Stagnation Pressure in Compressible Flow/(Gas Constant in Compressible Flow*Stagnation Density in Compressible Flow)
T_s = p_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 Temperature considering other Stagnation Properties of Fluid?

Stagnation Temperature considering other Stagnation Properties of Fluid calculator uses Stagnation Temperature in Compressible Flow = Stagnation Pressure in Compressible Flow/(Gas Constant in Compressible Flow*Stagnation Density in Compressible Flow) to calculate the Stagnation Temperature in Compressible Flow, The Stagnation temperature considering other stagnation properties of fluid formula is known while considering the ratio of the stagnation pressure to the gas constant and the stagnation density. Stagnation Temperature in Compressible Flow is denoted by T_s symbol.

How to calculate Stagnation Temperature considering other Stagnation Properties of Fluid using this online calculator? To use this online calculator for Stagnation Temperature considering other Stagnation Properties of Fluid, enter Stagnation Pressure in Compressible Flow (p_s), Gas Constant in Compressible Flow (R) & Stagnation Density in Compressible Flow (ρ_s) and hit the calculate button. Here is how the Stagnation Temperature considering other Stagnation Properties of Fluid calculation can be explained with given input values -> 168.6031 = 122000/(287.14*2.52).

FAQ

What is Stagnation Temperature considering other Stagnation Properties of Fluid?

The Stagnation temperature considering other stagnation properties of fluid formula is known while considering the ratio of the stagnation pressure to the gas constant and the stagnation density and is represented as T_s = p_s/(R*ρ_s) or Stagnation Temperature in Compressible Flow = Stagnation Pressure in Compressible Flow/(Gas Constant in Compressible Flow*Stagnation Density in Compressible Flow). Stagnation Pressure in Compressible Flow is defined as the pressure 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 Temperature considering other Stagnation Properties of Fluid?

The Stagnation temperature considering other stagnation properties of fluid formula is known while considering the ratio of the stagnation pressure to the gas constant and the stagnation density is calculated using Stagnation Temperature in Compressible Flow = Stagnation Pressure in Compressible Flow/(Gas Constant in Compressible Flow*Stagnation Density in Compressible Flow). To calculate Stagnation Temperature considering other Stagnation Properties of Fluid, you need Stagnation Pressure in Compressible Flow (p_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 Pressure 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 Temperature in Compressible Flow?

In this formula, Stagnation Temperature in Compressible Flow uses Stagnation Pressure 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 Temperature in Compressible Flow = Temperature of Still Air*(1+(Specific Heat Ratio-1)/2*Mach Number for Compressible Flow^2)

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