Two uniformly distributed loads of w = 3500 lb/ftact on the simply supported beam shown in Figure A. The beam spans are a = 7.3 ft and L = 18.0 ft. The beam cross section shown in Figure B has dimensions of b₁ = 16.25 in., d₁ = 5.50 in., b₂ = 9.00 in., and d₂ = 11.75 in. Calculate the maximum tensile and compressive bending stresses produced in segment BC of the beam. A W a FIGURE A FIGURE B otensile = compressive = d₁ d₂ B i IN MI L b₁ b₂ C W a psi psi D X
Two uniformly distributed loads of w = 3500 lb/ftact on the simply supported beam shown in Figure A. The beam spans are a = 7.3 ft and L = 18.0 ft. The beam cross section shown in Figure B has dimensions of b₁ = 16.25 in., d₁ = 5.50 in., b₂ = 9.00 in., and d₂ = 11.75 in. Calculate the maximum tensile and compressive bending stresses produced in segment BC of the beam. A W a FIGURE A FIGURE B otensile = compressive = d₁ d₂ B i IN MI L b₁ b₂ C W a psi psi D X
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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Question
Do not roundoff the values during computation.
![Two uniformly distributed loads of w = 3500 lb/ftact on the simply supported beam shown in Figure A. The beam spans are a = 7.3
ft and L = 18.0 ft. The beam cross section shown in Figure B has dimensions of b₁ = 16.25 in., d₁ = 5.50 in., b₂ = 9.00 in., and
d₂ = 11.75 in. Calculate the maximum tensile and compressive bending stresses produced in segment BC of the beam.
A
W
a
FIGURE A
FIGURE B
otensile =
compressive
=
d₁
d₂
B
i
IM
L
b₁
b₂
C
W
a
psi
psi
D
X](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F9de751ce-d0b4-477e-8168-a98ebf0c920e%2Fb72e28b2-28ed-4255-bfeb-f4c85dce9b27%2Fal2t60n_processed.jpeg&w=3840&q=75)
Transcribed Image Text:Two uniformly distributed loads of w = 3500 lb/ftact on the simply supported beam shown in Figure A. The beam spans are a = 7.3
ft and L = 18.0 ft. The beam cross section shown in Figure B has dimensions of b₁ = 16.25 in., d₁ = 5.50 in., b₂ = 9.00 in., and
d₂ = 11.75 in. Calculate the maximum tensile and compressive bending stresses produced in segment BC of the beam.
A
W
a
FIGURE A
FIGURE B
otensile =
compressive
=
d₁
d₂
B
i
IM
L
b₁
b₂
C
W
a
psi
psi
D
X
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