The frame in (Figure 1) supports a centrally applied distributed load of 1.8 kip/ft. The pins at C and D are at the same location as the neutral axis for the cross section. Figure 12 ft -5- C ↓↓↓↓↓↓ A1.5 in. HH 3 in. 3 in. B 1 in. 6 in. 16 ft 1.8 kip/ft D ▼ Part A Determine the state of stress at point A on member CD. Enter your answers in kilopounds per square inch to three significant figures separated by a comma. Enter negative value for the normal stress in the case of compression and positive value in the case of tension. 195] ΑΣΦ.It vec σATA= Part B OB. TB = ? Determine the state of stress at point B on member CD. Enter your answers in kilopounds per square inch to three significant figures separated by a comma. Enter negative value for the normal stress in the case of compression and positive value in the case of tension. AΣo↓ vec 4 ksi ? ksi
The frame in (Figure 1) supports a centrally applied distributed load of 1.8 kip/ft. The pins at C and D are at the same location as the neutral axis for the cross section. Figure 12 ft -5- C ↓↓↓↓↓↓ A1.5 in. HH 3 in. 3 in. B 1 in. 6 in. 16 ft 1.8 kip/ft D ▼ Part A Determine the state of stress at point A on member CD. Enter your answers in kilopounds per square inch to three significant figures separated by a comma. Enter negative value for the normal stress in the case of compression and positive value in the case of tension. 195] ΑΣΦ.It vec σATA= Part B OB. TB = ? Determine the state of stress at point B on member CD. Enter your answers in kilopounds per square inch to three significant figures separated by a comma. Enter negative value for the normal stress in the case of compression and positive value in the case of tension. AΣo↓ vec 4 ksi ? ksi
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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Question

Transcribed Image Text:The frame in (Figure 1) supports a centrally applied distributed
load of 1.8 kip/ft. The pins at C and D are at the same
location as the neutral axis for the cross section.
Figure
12 ft
-5ft-
C
A
O
B
E
HH
3 in. 3 in.
1 in.
B
1.5 in.
6 in.
16 ft
1.8 kip/ft
D
Part A
Determine the state of stress at point A on member CD.
Enter your answers in kilopounds per square inch to three significant figures separated by a comma. Enter negative
value for the normal stress in the case of compression and positive value in the case of tension.
σA, TA=
Part B
OB, TB =
VO
Avec
Determine the state of stress at point B on member CD.
Enter your answers in kilopounds per square inch to three significant figures separated by a comma. Enter negative
value for the normal stress in the case of compression and positive value in the case of tension.
[VD
?
ΑΣΦ
ΑΣΦΠ 1 vec
ksi
?
ksi
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Step 1: Determine the reaction forces at C and D.
VIEWStep 2: Evaluate the internal forces acting in bar CD at section 5 ft from support C.
VIEWStep 3: Evaluate properties of T-section
VIEWStep 4: Evaluate resultant normal stress acting on cross-section due to axial force and bending moment.
VIEWStep 5: Evaluate resultant shear stress acting on cross-section due to shear force.
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