“…It should be noticed that Fig. 3 also shows that a large pressure gradient almost in parallel to the y-axis exists at about x = 1.0, 2.8 and 4.2 m, which were not obtained with the past two-dimensional analysis [3]. illustrates a distribution of the static pressure on the x-z plane (y = 0), where it can be clearly shown that strong oblique shock waves are generated at the connection between the nozzle and the insulating walls, traveling down to the channel exit.…”