Table 1 reports the stagnation temperature on the cylinder. This resulted in some strange behavior in the subsonic portion of the boundary layer at the outflow boundaries. This can be seen in the velocity vectors of Fig. 2 and Fig. This was probably due to the fact that the freestream pressure was being used for those points, which is incorrect. This case is still being worked on.
Plans are to include chemistry models for a more realistic simulation.
A plot of the velocity vectors. A plot of the velocity vectors. The data files and results. Temperature Calorically Perfect hc. This page was last updated on December 31, 1997.