689/CH8/EX8.7/7.sce


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clc; funcprot(0);
//Example 8.7  Lift Drag Ratio 

// Initialisation of variables
W = 5000;
LD_Max = 21.5;

// Calculations
D = W/LD_Max;

//Results 
disp(D,"Minimum drag on clark Y wing (lb)");