“…Without entering into the difficult analysis of the supercritical flow solution, we attempt to set up a criterion that can predict whether or not for given initial reservoir conditions, nozzle geometry and Q~,,(x) the flow is supercritical. We restrict our discussion to supersonic heat addition (Xb > O) because subsonic heat addition (Xb < 0) requires the influence of the exit boundary conditions as well [for numerical solution of the differential theory with heat addition in the subsonic region see Jungclaus and van Raay (1967)]. It follows at once from Proposition 2.2.2 that the flow is subcritical if…”