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

Structural Analysis
6th Edition
ISBN:9781337630931
Author:KASSIMALI, Aslam.
Publisher:KASSIMALI, Aslam.
Chapter9: Application Of Influence Lines
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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
Transcribed Image Text: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
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