Vinay Mishra
Indian Institute for Aeronautical Engineering and Information Technology (IIAEIT), Pune
Vinay Mishra has created this Calculator and 300+ more calculators!
Maiarutselvan V
PSG College of Technology (PSGCT), Coimbatore
Maiarutselvan V has verified this Calculator and 200+ more calculators!

11 Other formulas that you can solve using the same Inputs

Stanton Number (using basic fluid properties)
Stanton Number=External convection heat transfer coefficient/(Specific Heat Capacity*Fluid Velocity*Density) GO
Heat Loss due to Pipe
Heat Loss due to Pipe=(Force*Length*Fluid Velocity^2)/(2*Diameter *Acceleration Due To Gravity) GO
Cavitation Number
Cavitation number=(Pressure-Vapour pressure)/(mass density*(Fluid Velocity^2)/2) GO
Head Loss due to friction
Head loss=Darcy friction factor*Fluid Velocity^(2)*Length/(Pipe Diameter*2*[g]) GO
Reynolds Number for Non-Circular Tubes
Reynolds Number=Density*Fluid Velocity*Characteristic Length/Dynamic viscosity GO
Reynolds Number
Reynolds Number=Liquid Density*Fluid Velocity*Pipe Diameter/Dynamic viscosity GO
Dynamic Pressure head-pitot tube
Dynamic Pressure head=(Fluid Velocity^(2))/(2*Acceleration Due To Gravity) GO
Reynolds Number for Circular Tubes
Reynolds Number=Density*Fluid Velocity*Diameter /Dynamic viscosity GO
Inertial Force Per Unit Area
Inertial Force per unit area=(Fluid Velocity^2)*Density GO
Dynamic Pressure
Dynamic Pressure=(Liquid Density*Fluid Velocity^(2))/2 GO
Turbulence
Turbulence=Density*Dynamic viscosity*Fluid Velocity GO

2 Other formulas that calculate the same Output

Stagnation temperature considering the compressible fluid flow
Stagnation Temperature=Temperature of wall 1*(1+(((Specific Heat Ratio-1)/2)*(Local Mach number^2))) GO
Stagnation temperature considering other stagnation properties of the fluid
Stagnation Temperature=Stagnation Pressure/(Gas Constant*Stagnation density ) GO

Stagnation Temperature Formula

Stagnation Temperature=Static Temperature+((Fluid Velocity^2)/(2*Specific Heat Capacity at Constant Pressure))
T<sub>0</sub>=T+((u<sub>f</sub>^2)/(2*C<sub>p</sub>))
More formulas
Speed of Sound GO
Mach Number GO
Mach Angle GO
Mayer's formula GO
Thermal resistance for conduction through 2 resistances in parallel GO
Isentropic compressibility for given density and speed of sound GO

What is a stagnation condition?

In fluid dynamics, a stagnation point is a point in a flow field where the local velocity of the fluid is zero.

Why is stagnation temperature important?

The stagnation temperature is important because it is the temperature that occurs at a stagnation point on the object.

How to Calculate Stagnation Temperature?

Stagnation Temperature calculator uses Stagnation Temperature=Static Temperature+((Fluid Velocity^2)/(2*Specific Heat Capacity at Constant Pressure)) to calculate the Stagnation Temperature, The Stagnation Temperature is defined as the total temperature at all points on the streamline leading to the stagnation point and depends upon the velocity at the point of interest along the stagnation streamline. Stagnation Temperature and is denoted by T0 symbol.

How to calculate Stagnation Temperature using this online calculator? To use this online calculator for Stagnation Temperature, enter Static Temperature (T), Fluid Velocity (uf) and Specific Heat Capacity at Constant Pressure (Cp) and hit the calculate button. Here is how the Stagnation Temperature calculation can be explained with given input values -> 10.0625 = 10+((1^2)/(2*8)).

FAQ

What is Stagnation Temperature?
The Stagnation Temperature is defined as the total temperature at all points on the streamline leading to the stagnation point and depends upon the velocity at the point of interest along the stagnation streamline and is represented as T0f^2)/(2*Cp)) or Stagnation Temperature=Static Temperature+((Fluid Velocity^2)/(2*Specific Heat Capacity at Constant Pressure)). The Static Temperature is defined as the temperature of the gas if it had no ordered motion and was not flowing, Fluid velocity is the volume of fluid flowing in the given vessel per unit cross sectional area and Specific heat capacity at constant pressure means the amount of heat that is required to raise the temperature of a unit mass of gas by 1 degree at constant pressure.
How to calculate Stagnation Temperature?
The Stagnation Temperature is defined as the total temperature at all points on the streamline leading to the stagnation point and depends upon the velocity at the point of interest along the stagnation streamline is calculated using Stagnation Temperature=Static Temperature+((Fluid Velocity^2)/(2*Specific Heat Capacity at Constant Pressure)). To calculate Stagnation Temperature, you need Static Temperature (T), Fluid Velocity (uf) and Specific Heat Capacity at Constant Pressure (Cp). With our tool, you need to enter the respective value for Static Temperature, Fluid Velocity and Specific Heat Capacity at Constant 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 Stagnation Temperature?
In this formula, Stagnation Temperature uses Static Temperature, Fluid Velocity and Specific Heat Capacity at Constant Pressure. We can use 2 other way(s) to calculate the same, which is/are as follows -
  • Stagnation Temperature=Stagnation Pressure/(Gas Constant*Stagnation density )
  • Stagnation Temperature=Temperature of wall 1*(1+(((Specific Heat Ratio-1)/2)*(Local Mach number^2)))
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