project - W plot(y,W1 hold on plot(y,W2'r...

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function[] = project() f %Knowns % hb=1540; %half span b=hb*2; Wg=350000; %gross weight of aircraft n=2.81366; %load factor n %linear case % y=[0:1540]; W1=1278.94-.83048*y; W %ellipse % W0=814.196 W2=sqrt(W0.^2-W0.^2*y.^2./(hb).^2); W %Average case % W0=994.973 W3=1/2.*((W0).*(1-1./hb.*y)+sqrt((W0).^2-(W0).^2.*y.^2./(hb)^2));
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Unformatted text preview: W plot(y,W1) hold on plot(y,W2,'r') plot(y,W3,'m',xlabel ('wing span (in)'),ylabel ('lift/unit span (lb/in)')) p hold off %axes('position',[0,0,1540,1278.94]) %...
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This note was uploaded on 08/27/2011 for the course AEROSPACE 3115C taught by Professor Bakcer during the Spring '10 term at University of Florida.

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