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.
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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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](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F13d1e7e1-7718-43f3-9c51-b404da2a25b4%2F4820b512-938a-41aa-86ae-39a6dbf2b838%2Ffbp5pzc_processed.jpeg&w=3840&q=75)
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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