Repeat problem 11.1, except consider a nozzle with a finite expansion section which is a circular arc with an equal to three throat heights. Compare this nozzle contour and total length with the minimum-length nozzle of problem 11.1.

Data From Problem 11.1:

Using the method of characteristics, compute and graph the contour of a two-dimensional minimum-length nozzle for the expansion of air to a design exit Mach number of 2.