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.

Elements Of Electromagnetics
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ISBN:9780190698614
Author:Sadiku, Matthew N. O.
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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
WojciechBeczynski / Shutterstock com
Transcribed Image Text: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 WojciechBeczynski / Shutterstock com
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