airspeed = 50		//Create a an airspeed variable
myCell = cell(11,1,2)	//Allocate an array to hold 22 force and drag values

for k = 1:11
	myCell(k,1,1) = (0.5)*(1.225 kg/m^3)*(airspeed)^2*(427.8)*(2.3)
	myCell(k,1,1) = (0.5)*(1.225 kg/m^3)*(airspeed)^2*(427.8)*(0.15)
	airspeed = airspeed + 20
end

fprintf("For a true airspeed of 300: Lift:f%", myCell(11,1,1))
fprintf("For a true airspeed of 300: Drag:f%", myCell(11,1,2))