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Ps An airplane with an elliptical lift distribution has the following characteristics: Wing loading =1382N/m2 U =83m/sat altitude of 3600mAR=7S=11m2 L=0=1.3Calculate values for: (i) the
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An airplane with an elliptical lift distribution has the following characteristics: Wing loading =1382N/m2U=83m/sat altitude of 3600mAR=7S=11m2L=0=1.3Calculate values for: (i) the circulation in the plane of symmetry (ii) the induced and effective angle
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