A simply supported beam hinged at A and supported at C, is carrying a distributed load and a point load (see Fig. 1). The beam has a Young Modulus E = 80 GPa and a constant depth of 400 mm. The moment of inertia of the beam is limited to be l = 255 x 10-4 m. P= 120 KN 9 15 KN/m 4 (m) 2 (m) Figure 1 (V) Derive the deflection equation and find the value of the integration constants. (vi) Find the deflection at D.
A simply supported beam hinged at A and supported at C, is carrying a distributed load and a point load (see Fig. 1). The beam has a Young Modulus E = 80 GPa and a constant depth of 400 mm. The moment of inertia of the beam is limited to be l = 255 x 10-4 m. P= 120 KN 9 15 KN/m 4 (m) 2 (m) Figure 1 (V) Derive the deflection equation and find the value of the integration constants. (vi) Find the deflection at D.
Mechanics of Materials (MindTap Course List)
9th Edition
ISBN:9781337093347
Author:Barry J. Goodno, James M. Gere
Publisher:Barry J. Goodno, James M. Gere
Chapter9: Deflections Of Beams
Section: Chapter Questions
Problem 9.5.1P: A simply supported beam (E = 1600 ksi) is loaded by a triangular distributed load from A to C(see...
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![A simply supported beam hinged at A and supported at C, is carrying a distributed load and
a point load (see Fig. 1). The beam has a Young Modulus E = 80 GPa and a constant
depth of 400 mm. The moment of inertia of the beam is limited to be l =
255 x 10-4 m*.
P- 120 KN
9 15 KN/m
4 m)
4 (m)
2 (m)
Figure 1
(V) Derive the deflection equation and find the value of the integration constants.
(vi)
Find the deflection at D.](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2Fa4d05f05-bde1-4e45-8632-80b7f1d93381%2F345e19a1-899d-4265-968a-196872a130b8%2Ffi2nrpe_processed.jpeg&w=3840&q=75)
Transcribed Image Text:A simply supported beam hinged at A and supported at C, is carrying a distributed load and
a point load (see Fig. 1). The beam has a Young Modulus E = 80 GPa and a constant
depth of 400 mm. The moment of inertia of the beam is limited to be l =
255 x 10-4 m*.
P- 120 KN
9 15 KN/m
4 m)
4 (m)
2 (m)
Figure 1
(V) Derive the deflection equation and find the value of the integration constants.
(vi)
Find the deflection at D.
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