Question

Prob. 6-1 6-2 The dead-weight loading along the centerline of the airplane wing is shown. If the wing is fixed to the fuselage at A. determine the reactions at A, and then draw the shear and moment diagram for the wing. sup 6 kN/m 15 kN 3.75 kN/m A 0.6 m 2.4 m 0.9 m 75 kN Prob. 6-2 6-3 Draw the shear and moment diagrams for the overhang beam. 8 kN/m

why 2.3 ?

Answer 1

BOlutoo Noco, daaw the moment diagoam Shear ana FO the wing 6KNm 3-75KNAn 15KN RvA RA RHA .um a6m 75 kN 58-98KN Shear porce 8./875 KN +ve aiag yam -ye 22.02k 29.5875 kn-g Bending moment aagra m -ve 3.6k 16 099 KN-m + (a7s xk5) + /-5X2-25) +5 RVA +75 +(G-E RvA+75-11 8a5 +15 RVA +75 8R5 Scanned with CamScanner CS

Res +76 = २६. 8२5 RA 26-885-76 Coloran oard bedirection) RIA --48.1875 kN Now) the momentom EMA x-4x375x3)-ISXS-(3-75x1:5 Ko 75)- x5x5KOS + 75x09 +MA 0 -37-9125 +67.5+HAO MA =-67-5+37.9145 29.58 75 kN-m MA ur o atle CS CamScanner Scanned with