(а) 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) WojciechBeczynski / Shu ttersto ck.com

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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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 Vand bending moment M at 4 m from the tip of the wing.

(а)
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)
WojciechBeczynski / Shu ttersto ck.com
Transcribed Image Text:(а) 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) WojciechBeczynski / Shu ttersto ck.com
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