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+//Example 4_12
+clc;funcprot(0);
+//Given data
+p_a=1.30;// Atmospheric pressure in bar
+p_c=0.5;// bar
+V_c=5;// m/sec
+V_d=2;// m/sec
+h_f=0.2;// m
+g=9.81;// m/s^2
+
+//Calculation
+w=1000*9.81;// N
+h=(((p_a-p_c)*1.03*10^5)/w)-((V_c^2)/(2*g))+(((V_d^2)/(2*g))+h_f);// m
+printf('\n The maximum height of the turbine above tail race,h=%0.3f m',h);
+// The answer provided in the textbook is wrong