Above Mach 1, You Must Widen to Speed Up — The Laval Nozzle Paradox
·7 min read
Area ratio 2.5 exits near Mach 2.44 on the supersonic branch, static pressure at 6.3 percent of stagnation. Raise back pressure and a shock stands inside.
Area ratio 2.5 exits near Mach 2.44 on the supersonic branch, static pressure at 6.3 percent of stagnation. Raise back pressure and a shock stands inside.