void arckarcp(double g, double m, double cin, double result[3], int *ierr);
Compute the Karman-Tsien pressure correction coefficient relations given the mach number and the the incompressebility coefficient .
ENTRY: Specific heat constant .
ENTRY: Mach number .
ENTRY: Incompressebility coefficient .
EXIT: Array with result properties as described in 18.
EXIT: (optional) Return status code.
Specific heat ratio .
Given out of range.