*1-12. The serving tray T used on an airplane is supported on each side by an arm. The tray is pin connected to the arm at A, and at B there is a smooth pin. (The pin can move within the slot in the arms to permit folding the tray against the front passenger seat when not in use.) Determine the resultant internal loadings acting on the cross section of the arm through point C when the tray arm supports the loads shown. 12 N 9N |-100 mm- A 15 mm -150 mm В 60° T 500 mm Vc Mc
*1-12. The serving tray T used on an airplane is supported on each side by an arm. The tray is pin connected to the arm at A, and at B there is a smooth pin. (The pin can move within the slot in the arms to permit folding the tray against the front passenger seat when not in use.) Determine the resultant internal loadings acting on the cross section of the arm through point C when the tray arm supports the loads shown. 12 N 9N |-100 mm- A 15 mm -150 mm В 60° T 500 mm Vc Mc
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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Transcribed Image Text:*1-12. The serving tray T used on an airplane is supported
on each side by an arm. The tray is pin connected to the arm
at A, and at B there is a smooth pin. (The pin can move within
the slot in the arms to permit folding the tray against the
front passenger seat when not in use.) Determine the
resultant internal loadings acting on the cross section of
the arm through point C when the tray arm supports the
loads shown.
12 N
9N
|-100 mm-
A
15 mm
-150 mm
В
60°
T
500 mm
Vc
Mc
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