Calculate stagnation temperature and isentropic total-to-static ratios for compressible flow.
Stagnation temperature
396.00 K
T0/T 1.8000
Pressure ratio
7.8244
p0/p
Density ratio
4.3469
rho0/rho
Flow brought to rest at a probe converts kinetic energy into total temperature under the isentropic model.
M 2.00
Temperature ratio
T0/T 1.8000
gamma 1.40 isentropic flow
Pressure ratio
p0/p 7.824
total pressure from the same state
Density ratio
rho0/rho 4.347
follows from p0/T0 relation
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Calculate stagnation temperature and isentropic total-to-static ratios for compressible flow.
Stagnation temperature
396.00 K
T0/T 1.8000
Pressure ratio
7.8244
p0/p
Density ratio
4.3469
rho0/rho
Flow brought to rest at a probe converts kinetic energy into total temperature under the isentropic model.
M 2.00
Temperature ratio
T0/T 1.8000
gamma 1.40 isentropic flow
Pressure ratio
p0/p 7.824
total pressure from the same state
Density ratio
rho0/rho 4.347
follows from p0/T0 relation
This tool is open source and the underlying logic is fully transparent. You can inspect the code, understand the calculations, and contribute improvements. If you want to use the tool in your own website, course page, or learning platform, you can also embed it directly and start from a ready-made iframe setup for this exact tool.
Open source: review the implementation and see how the results are produced.
Embeddable: preview this tool, copy the iframe, and use it in your own site or LMS.