4.3-10 Under cruising conditions, the distributed load aeting on the wing of a small airplane has the idealized variation shown in the figure. Calculate the shear force V and bending moment M at 4 m from the tip of the wing.

4.3-10 Under cruising conditions, the distributed load aeting on the wing of a small airplane has the idealized variation shown in the figure. Calculate the shear force V and bending moment M at 4 m from the tip of the wing.

Mechanics of Materials (MindTap Course List)

9th Edition

ISBN:9781337093347

Author:Barry J. Goodno, James M. Gere

Publisher:Barry J. Goodno, James M. Gere

Chapter1: Tension, Compression, And Shear

Section: Chapter Questions

Problem 1.3.22P: Find support reactions at A and D and then calculate the axial force N. shear force 1 and bending...

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Concept explainers

Bending Moment

In general, we can define the bending moment as the reaction induced when a certain amount of load or force is applied to an element which makes it bend.

Question

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4.3-10 Under cruising conditions, the distributed
load acting on the wing of a small airplane has the
idealized variation shown in the figure.
Calculate the shear force V and bending
moment M at 4 m from the tip of the wing.
(a)
Wings of a small airplane have distributed uplift loads.
1600 N/m
900 N/m
1.0 m
2.6 m
2.6 m
(b)
PROBLEM 4.3-10
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