Stagnation Temperature considering Compressible Fluid Flow Calculator

✖Temperature of Still Air is the temperature of the nonflowing air with zero velocity.ⓘ Temperature of Still Air [T₁]			+10% -10%
✖The Specific Heat Ratio is the ratio of the heat capacity at constant pressure to heat capacity at constant volume of the flowing fluid for non-viscous and compressible flow.ⓘ Specific Heat Ratio [y]			+10% -10%
✖Mach Number For Compressible Flow is a dimensionless quantity in fluid dynamics representing the ratio of flow velocity past a boundary to the local speed of sound.ⓘ Mach Number For Compressible Flow [M]			+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 Compressible Fluid Flow [T_s]

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Stagnation Temperature considering Compressible Fluid Flow Solution

STEP 0: Pre-Calculation Summary

Formula Used

Stagnation Temperature in Compressible Flow = Temperature of Still Air*(1+(Specific Heat Ratio-1)/2*Mach Number For Compressible Flow^2)
T_s = T₁*(1+(y-1)/2*M^2)
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.
Temperature of Still Air - (Measured in Kelvin) - Temperature of Still Air is the temperature of the nonflowing air with zero velocity.
Specific Heat Ratio - The Specific Heat Ratio is the ratio of the heat capacity at constant pressure to heat capacity at constant volume of the flowing fluid for non-viscous and compressible flow.
Mach Number For Compressible Flow - Mach Number For Compressible Flow is a dimensionless quantity in fluid dynamics representing the ratio of flow velocity past a boundary to the local speed of sound.

STEP 1: Convert Input(s) to Base Unit

Temperature of Still Air: 240 Kelvin --> 240 Kelvin No Conversion Required
Specific Heat Ratio: 1.4 --> No Conversion Required
Mach Number For Compressible Flow: 1.24 --> No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

T_s = T₁*(1+(y-1)/2*M^2) --> 240*(1+(1.4-1)/2*1.24^2)

Evaluating ... ...

T_s = 313.8048

STEP 3: Convert Result to Output's Unit

313.8048 Kelvin --> No Conversion Required

FINAL ANSWER

313.8048 Kelvin <-- Stagnation Temperature in Compressible Flow

(Calculation completed in 00.004 seconds)

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Created by Maiarutselvan V

PSG College of Technology (PSGCT), Coimbatore

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< 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 Temperature considering Compressible Fluid Flow Formula

LaTeX Go

Stagnation Temperature in Compressible Flow = Temperature of Still Air*(1+(Specific Heat Ratio-1)/2*Mach Number For Compressible Flow^2)
T_s = T₁*(1+(y-1)/2*M^2)

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.

What is the significance of Mach number in compressible fluid flow?

The Mach Number is a dimensionless value useful for analyzing fluid flow dynamics problems where compressibility is a significant factor. The bulk modulus elasticity has the dimension pressure and is commonly used to characterize fluid compressibility. The square of the Mach number is the Cauchy Number.

How to Calculate Stagnation Temperature considering Compressible Fluid Flow?

Stagnation Temperature considering Compressible Fluid Flow calculator uses Stagnation Temperature in Compressible Flow = Temperature of Still Air*(1+(Specific Heat Ratio-1)/2*Mach Number For Compressible Flow^2) to calculate the Stagnation Temperature in Compressible Flow, Stagnation Temperature considering Compressible Fluid Flow refers to the total temperature of the fluid when it comes to rest under stagnation conditions. This parameter is essential in aerodynamics, gas dynamics, and thermodynamics for understanding the thermal energy state of the fluid at critical points such as inlets and outlets of nozzles or turbines. It is influenced by factors such as stagnation pressure, density, and velocity, and plays a crucial role in designing and analyzing propulsion systems, combustion processes, and high-speed fluid dynamics. Stagnation Temperature in Compressible Flow is denoted by T_s symbol.

How to calculate Stagnation Temperature considering Compressible Fluid Flow using this online calculator? To use this online calculator for Stagnation Temperature considering Compressible Fluid Flow, enter Temperature of Still Air (T₁), Specific Heat Ratio (y) & Mach Number For Compressible Flow (M) and hit the calculate button. Here is how the Stagnation Temperature considering Compressible Fluid Flow calculation can be explained with given input values -> 313.8048 = 240*(1+(1.4-1)/2*1.24^2).

FAQ

What is Stagnation Temperature considering Compressible Fluid Flow?

Stagnation Temperature considering Compressible Fluid Flow refers to the total temperature of the fluid when it comes to rest under stagnation conditions. This parameter is essential in aerodynamics, gas dynamics, and thermodynamics for understanding the thermal energy state of the fluid at critical points such as inlets and outlets of nozzles or turbines. It is influenced by factors such as stagnation pressure, density, and velocity, and plays a crucial role in designing and analyzing propulsion systems, combustion processes, and high-speed fluid dynamics and is represented as T_s = T₁*(1+(y-1)/2*M^2) or Stagnation Temperature in Compressible Flow = Temperature of Still Air*(1+(Specific Heat Ratio-1)/2*Mach Number For Compressible Flow^2). Temperature of Still Air is the temperature of the nonflowing air with zero velocity, The Specific Heat Ratio is the ratio of the heat capacity at constant pressure to heat capacity at constant volume of the flowing fluid for non-viscous and compressible flow & Mach Number For Compressible Flow is a dimensionless quantity in fluid dynamics representing the ratio of flow velocity past a boundary to the local speed of sound.

How to calculate Stagnation Temperature considering Compressible Fluid Flow?

Stagnation Temperature considering Compressible Fluid Flow refers to the total temperature of the fluid when it comes to rest under stagnation conditions. This parameter is essential in aerodynamics, gas dynamics, and thermodynamics for understanding the thermal energy state of the fluid at critical points such as inlets and outlets of nozzles or turbines. It is influenced by factors such as stagnation pressure, density, and velocity, and plays a crucial role in designing and analyzing propulsion systems, combustion processes, and high-speed fluid dynamics is calculated using Stagnation Temperature in Compressible Flow = Temperature of Still Air*(1+(Specific Heat Ratio-1)/2*Mach Number For Compressible Flow^2). To calculate Stagnation Temperature considering Compressible Fluid Flow, you need Temperature of Still Air (T₁), Specific Heat Ratio (y) & Mach Number For Compressible Flow (M). With our tool, you need to enter the respective value for Temperature of Still Air, Specific Heat Ratio & Mach Number For 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 Temperature of Still Air, Specific Heat Ratio & Mach Number For Compressible Flow. We can use 1 other way(s) to calculate the same, which is/are as follows -

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

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