The simply supported beam consists of a W530 × 66 structural steel wide-flange shape [E = 200 GPa; I = 351 × 106 mm4]. Assume w = 45 kN/m, L1 = 2.6 m, and L2 = 2.6 m. For the loading shown, determine: (a) the beam deflection at point B. (b) the beam deflection at point D. Determine the component of the beam deflection at point B due to only the portion of the uniformly distributed load w between the supports at point A and point C. Answer: vB1 = mm. Part 2 Determine the magnitude of the bending moment at point C (report a positive number) due to only the portion of the uniformly distributed load w between point C and point D. Answer: MC = kN-m. Part 3 Determine the component of the beam deflection at point B due to the moment produced at point C by the portion of the uniformly distributed load w between point C and point D. Answer: vB2 = mm

Structural Analysis
6th Edition
ISBN:9781337630931
Author:KASSIMALI, Aslam.
Publisher:KASSIMALI, Aslam.
Chapter10: Analysis Of Symmetric Structures
Section: Chapter Questions
Problem 16P
icon
Related questions
Question

The simply supported beam consists of a W530 × 66 structural steel wide-flange shape [E = 200 GPa; I = 351 × 106 mm4]. Assume w = 45 kN/m, L1 = 2.6 m, and L2 = 2.6 m. For the loading shown, determine:
(a) the beam deflection at point B.
(b) the beam deflection at point D.

Determine the component of the beam deflection at point B due to only the portion of the uniformly distributed load w between the supports at point A and point C.

Answer: vB1 =          mm.

Part 2

Determine the magnitude of the bending moment at point C (report a positive number) due to only the portion of the uniformly distributed load w between point C and point D.
Answer: MC =          kN-m.
 

Part 3

Determine the component of the beam deflection at point B due to the moment produced at point C by the portion of the uniformly distributed load w between point C and point D.
Answer: vB2 =   mm.
 

Part 4

Determine the total beam deflection at point B due to the combined effects of the uniformly distributed load w between the supports at point A and point C and the uniformly distributed load w between point C and point D.

Answer: vB =              mm.
 

Part 5

Determine the component of the rotation angle of the beam at point C due to only the portion of the uniformly distributed load w between the supports at point A and point C.

Answer: θC1=         rad.
 

Part 6

Determine the component of the beam deflection at point D produced by the component of the rotation angle of the beam at point C due to only the portion of the uniformly distributed load w between the supports at point A and point C.

Answer: vD1 =          mm.

Part 7

Determine the component of the beam rotation angle at point C due to the moment produced at point C by the portion of the uniformly distributed load w between point C and point D.

Answer: θC2=          rad.
 

Part 8

Determine the component of the beam deflection at point D due to the moment produced at point C by the portion of the uniformly distributed load w between point C and point D.

Answer: vD2 =           mm.
 

Part 9

Determine the cantilever deflection of the beam at point D due to the portion of the uniformly distributed load w between point C and point D. This is the deflection that would be calculated at point D assuming a fixed support at C and the distributed load w between C and D.

Answer: vD3 =           mm.
 
 

Part 10

Determine the total beam deflection at point D.

Answer: vD =          mm.
 
C
D
B
A
L1
L2
L,
Transcribed Image Text:C D B A L1 L2 L,
Expert Solution
trending now

Trending now

This is a popular solution!

steps

Step by step

Solved in 3 steps with 3 images

Blurred answer
Knowledge Booster
Methods to Determine Vertical Stress
Learn more about
Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, civil-engineering and related others by exploring similar questions and additional content below.
Recommended textbooks for you
Structural Analysis
Structural Analysis
Civil Engineering
ISBN:
9781337630931
Author:
KASSIMALI, Aslam.
Publisher:
Cengage,
Engineering Fundamentals: An Introduction to Engi…
Engineering Fundamentals: An Introduction to Engi…
Civil Engineering
ISBN:
9781305084766
Author:
Saeed Moaveni
Publisher:
Cengage Learning
Materials Science And Engineering Properties
Materials Science And Engineering Properties
Civil Engineering
ISBN:
9781111988609
Author:
Charles Gilmore
Publisher:
Cengage Learning