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+clc;
+clear all;
+disp("Boundary layer thickness")
+
+x=1.2;//m distance from the leading edge of plate
+v=15.4*10^(-6);//m^2/s kinematic viscocity
+U=2.8;//m/s velocity of air
+
+
+Re=U*x/v;// Reynold's number
+disp("Blasius solution")
+delta1=5*x*1000/(Re)^0.5;//mm
+disp("mm",delta1,"Maximum thickness of boundary layer =")
+
+Cfx1=0.664/(Re)^0.5;
+disp(Cfx1,"drag coefficient =")
+
+disp("Approximate solution")
+delta2=4.64*x*1000/(Re)^0.5;//mm
+disp("mm",delta2,"Maximum thickness of boundary layer =")
+Cfx2=0.646/(Re)^0.5;
+disp(Cfx2,"drag coefficient =")
+
+e1=(1-delta2/delta1)*100;
+disp("%",e1,"Deviation for delta =")
+
+e2=(1-Cfx2/Cfx1)*100;
+disp("%",e2,"Deviation for Drag coefficient =")