armcrkt - Critical mach number given Cp0 using Karman-Tsien pressure approximation

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3.4.5 armcrkt - Critical mach number given $Cp0$ using Karman-Tsien pressure approximation

double armcrkt(double g, double cp0, int *ierr);

Compute critical mach number given $Cp0$ Karman-Tsien pressure approximation.

Performance
Iterative

Arguments

G - REAL: ENTRY: Specific heat constant $γ$ .
CP0 - REAL: ENTRY: Critical pressure coefficent $C p0$ .
IERR - INTEGER: EXIT: (optional) Return status code.

Status codes

-1: Specific heat ratio $γ≤ 1$ .
-2: Iterative solver failed.

Return Value
Critical mach number $Mcrit$ or NAN on error.

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