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. 15 kN 6 kN/m 3.75 kN/m- 0,6 m -2.4 m -0.9 m- 75 kN
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. 15 kN 6 kN/m 3.75 kN/m- 0,6 m -2.4 m -0.9 m- 75 kN
Chapter9: Application Of Influence Lines
Section: Chapter Questions
Problem 2P
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