Project

Matlab program to calculate drag force

Objective: %clearing allclcclear allclose all %density in kg per metre cuberho = 1.2; % frontal area in metre squarea = 0.1; %velocitiesv = [1 : 100]; %drag coefficient for different shapescd1 = {'aerofoil', 'sphere', 'cube', 'flat plate'};cd2 = [0.05 0.47 1.05 1.28]; for i =1:4; CD1 = cd1(i); %accessing array element CD2 = cd2(i);…

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