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+clc
+// Example 5.5.py
+// Consider a convergent divergent duct with an exit to throat area ratio of 1.6.
+// Calculate the exit to reservoir pressure ratio required to achieve sonic flow
+// at the throat, but subsonic flow everywhere else.
+
+// Variable declaration
+Ae_by_At = 1.6 // ratio of exit to throat area
+
+// Calculations
+
+// since M = 1 at the throat Mt = Astar
+// Ae/At = Ae/Astar = 1.6
+
+// from table A1 for Ae/Astar = 1.6
+po_by_pe = 1.1117 // po/pe
+pe_by_po = 1/po_by_pe // pe/po
+
+
+// Results
+printf("\n Exit to reservoir required pressure ratio is %.1f", pe_by_po)
+