Stagnation temperature
T0 = T (1 + (gamma - 1) M^2 / 2)
Thermodynamics calculator
Estimate total temperature from static temperature, Mach number, and heat capacity ratio.
Calculator
Select units beside each input. Results update automatically.
Result
About this calculator
Stagnation temperature is the temperature a flowing gas would reach if brought to rest adiabatically.
Formulas
T0 = T (1 + (gamma - 1) M^2 / 2)
Worked example
T=288 K, M=0.8, gamma=1.4 gives 324.9 K
Guide
Reference
Total temperature of the moving gas.
Flow speed divided by local speed of sound.
Assumptions and limits
FAQ
Use these tools for education, screening, and early checks. Final work should use verified properties, standards, operating limits, and qualified engineering review.
Real systems include losses, non-ideal properties, transient behavior, two-phase effects, humidity assumptions, heat leaks, and measurement uncertainty.
Yes. Select units beside inputs where menus are shown. Values are converted internally before solving.
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