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authorprashantsinalkar2017-10-10 12:27:19 +0530
committerprashantsinalkar2017-10-10 12:27:19 +0530
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+//Solution 11-3
+WD=get_absolute_file_path('11_03_solution.sce');
+datafile=WD+filesep()+'11_03_example.sci';
+clc;
+exec(datafile)
+Re_L = V * L / nu; //Reynolds number at the end of the plate
+//determination of average friction coefficient
+if Re_L < Re_cr then
+ C_f = 1.328 * Re_L**-0.5; //for laminar flow at the end of the plate
+else
+ C_f = 0.074/ Re_L**0.2 - 1742/ Re_L; //for turbuent flow the end of the plate
+end
+F_D = C_f * L * rho * V**2 / 2; //drag force per unit width
+printf("The drag force acting on the top side of plate per unit width is %1.0f N.", F_D); \ No newline at end of file