Calculate thermodynamic properties across an isentropic flow. Isentropic flow is a flow process where entropy remains constant, which occurs in ideal compressible flow with no heat transfer or friction.
2.000
Supersonic flow
1.688
A/A* (ratio to sonic throat)
0.1278
p/p₀ (static to stagnation)
0.5556
T/T₀ (static to stagnation)
0.2300
ρ/ρ₀ (static to stagnation)
5.6404
p₀₂/p₀ (for supersonic with shock)
30.00°
μ = sin⁻¹(1/M) - Angle of Mach wave
26.38°
ν - Maximum turning angle for isentropic expansion
1.400
Gas: Air
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