Astar and T,p at the throat are only calculated if the flow is supersonic, otherwise it does not make sense. Bug detected in Me calculation with sympy (equation is wrong) and now sympy is struggling to solve solvetes
Astar and T,p at the throat are only calculated if the flow is supersonic, otherwise it does not make sense. Bug detected in Me calculation with sympy (equation is wrong) and now sympy is struggling to solve solvetes

MRod5/pyturb