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Assume a propeller blade is like a rod with moment of inertia given by 1 = 1/3 mL where the blade mass is 20 kg, and the dist
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05 0,5 mazobg I= 2m 12 = 2x20 (0-5) 40%-25 = 3.33 legim? {=20 T=3-33x2 = 6.66 N/m

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