Question

I Review Due to an unequal distribution of fuel in the wing tanks, the centers of gravity for the airplane fuselage A and wings B and C are located as shown. (Figure 1) Select the elements from the list and add them to the canvas setting the appropriate attributes, Submit Request Answer Part B Figure < 1 of 1 > If these components have weights W1 = 43000 lb , WB= 8000lb, and Wc = 6000lb, determine the normal reactions of the wheels D, E, and Fon the ground. Enter your answers numerically separated by commas. VAZD Iveco O2 ? No, No, NF- Submit Request Answer & ft 6 x 8 ft 20 ft 3 Provide Feedback Next > P Pearson

Answer 1

Taking Moment about y" Emy=0; 8000 llo 10 ,4300016 ND (8000X 4) +(43000) (4) +6000(4) - NF (27)=0 Nf=13.22222 kip Enzo; (8000) (6) - No (14) -6000 (8) + : NE (14)=0 NE (14) – NO CIW) = 0 0 NotNe +NE - 8000 - 6000 - 430000 NetND +132222222- 5700020 Ne tND = 43777.7778 → Solving 0& © NE - ND=0 NOENE 2 Nosnę : 43777-778 = 21.8888 KA No, No, NF = 21088, 2188, 13972 kipti