Stagnation Temperature Calculator

Stagnation Temperature (T₀):

Static Temperature (T):

Mach Number (M):

Ratio of Specific Heats (γ):

How This Is Calculated

$$ T_0 = T \left( 1 + \frac{\gamma - 1}{2} M^2 \right) $$ where:

T₀ = Stagnation Temperature (K)

T = Static Temperature (K)

M = Mach Number (Dimensionless)

γ = Ratio of Specific Heats (Dimensionless)

Assumptions

The fluid is compressible.
The flow is isentropic.
The system is in steady-flow.
The fluid behaves as an ideal gas.
There is no external work or heat transfer.

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Density Ratio