1 A beam shown in Figure 2.14a (Module 5, page 79) is made of T beam, determine maximum deflection if E = 4.09 x 10° MPa (for G-melina, stress grade 80, NSCP 2015) using area moment method P = 50KN P = 50KN A D B 2.0m 2.0m 2.0m Figure 2.14a

1 A beam shown in Figure 2.14a (Module 5, page 79) is made of T beam, determine maximum deflection if E = 4.09 x 10° MPa (for G-melina, stress grade 80, NSCP 2015) using area moment method P = 50KN P = 50KN A D B 2.0m 2.0m 2.0m Figure 2.14a

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

See similar textbooks

Related questions

Q: Obtain the shear forces in each beam.

A: Given

Q: 4. Find the lightest S-shape for the beam shown if the working stress in bending is 175 MPa. What is…

A: The given figure of beam is shown below:

Q: P3 P, P2 A 5-m long, simply supported beam is loaded as shown. Determine the lightest W-shape beam…

A: Given, There is a simply supported beam which is Loaded with point load and Udl as shown in the…

Q: For the beam shown below, Find the bending stress at point A. 50 kN 1.9 m 28 a 28 a 120 20 3 m 3 m

A: Since the unit of distance from top fibre is not mentioned we assumed to be 28 cm or .28 m The…

Q: a (Figure 1: A three cell section)

A: Since the section is symmetrical about horizontal axis. The strip is thin, so we can ignore it in…

Q: The ratio of the maximum deflections of a sim ply supported beam with a central load w and of a…

Q: Using the "Effects Overlay" of the original beam, using isostatic sub-beams and simulating them…

A: Given that :- Modulus of Elasticity (E) = 200 GPa = 200,000 MPaWeight of the beam (W) = 2.5 Applied…

Q: What will be the collapse load of the beam of uniform cross-section as shown in figure? W W/2 Mp Mp…

Q: The simply supported beam consists of a W460 × 82 structural steel wide-flange shape [E = 200 GPa; I…

Q: Problem 1: Calculate the axial stress in each part of this assembly if the ID of the steel tub…

Q: The simply supported beam consists of a W460 × 82 structural steel wide-flange shape [E = 200 GPa;…

A: Given Data: E=200 Gpa I=370*10^6 mm4 P=62 kN w=28 kn/m LAB=LBC=2.9 m LCD=1.9 m It is asked to…

Q: 1. Determine the nominal load P that will cause failure of the beam shown below. As part of your…

Q: The rigid platform shown has negligible mass and rests on two steel bars, each 250 mm long. The…

Q: if the maximum shear stress acting on rectangular beam is 50 N/mm, determine the average shear…

Q: Determine the stress concentration factor for the beam shown below that has a fillet to the larger…

A: step 1-

Q: 1. The structure shown below is subjected to a total uniform load w. The flexural stress in the…

A: (a) Consider the free body diagram of beam; For CDE; Re×L+w(1)22+w(1)22=0Re=0 Calculate shear at…

Q: 4. Find the lightest S-shape for the beam shown if the working stress in bending is 175 MPa. What is…

Q: What is the long-term deflection for dead load plus 45% permanent live load for 1 year, there is…

Q: A rigid platform in Figure MEC-208 has negligible mass carries a center load P and rests or two…

Q: An 8 m simple beam is loaded with a 208 kN point load at the first third of its length. The cross…

A: Given data: Load=208 kN Allowable stress=200 MPaThickness=20 mm Length=8m c=333.333 mm Load=208…

Q: The cantilever beam consists of a rectangular structural steel tube shape [E = 29,000 ksi; I = 1530…

Q: Notes: Attempt Five Question only Q1: For the composite structure shown in Fig.(1), determine the…

A: Composite structures are commonly known as Load-bearing elements which consist of elements like…

Q: A 20 mm diameter bar is 1.25 m long. When the bar is simply supported at its ends in a horizontal…

Q: Shape (E determine: (a) the beam deflection at point A. (b) the beam deflection at point B. Assume…

A: To find deflection at point A and B

Q: A 20 mm diameter bar is 1.25 m long. When the bar is simply supported at its ends in a horizontal…

Q: Use the F.E Method to draw a deformed shape and determine the max deflection and max bending stress…

Q: a) Is the beam properly reinforced/over-reinforced/ balanced Determine the factored moment…

A: RC Singly beam,b=500 mmD=700 mmd=600 mmf'c=48 MPaReinforcement: 3-30Mfy=400 MPaφc=0.65φs=0.85Es=2…

Q: Aluminum [E = 72 GPa] member ABC supports a load of 31 kN, as shown in the figure. Determine (a) the…

A: Given :

Q: A concrete beam pre-stressed with a parabolic tendon is shown in the figure. The eccentricity of the…

A: Given data Width of beam (B) = 500mm Depth of beam (D) = 750mm Pre stress force (P) = 1620 KN…

Q: Question 6 The reinforced concrete beam shown in Figure 6 is encastré at both ends. It supports a…

A: Calculation of vertical reactions

Q: Q2 The beam shown in Figure Q2 is loaded with a triangular distributed load from A to B, and a…

Q: A leaf spring is made of plates 50 mm wide and 8 mm thick. The spring has a span of 700 mm.…

Concept explainers

Beams

In structural engineering, a beam is a component made of a variety of materials (including steel alloys, and wood) that can resist loads applied laterally to the beam axis. Members, elements, rafters, shafts, and purlins are all terms used to describe beams.

Question

11.1 A beam shown in Figure 2.14a (Module 5, page 79) is made of T beam,
determine maximum deflection if E = 4.09 x 10° MPa (for G-melina, stress grade
80, NSCP 2015) using area moment method
200
P = 50KN
P = 50KN
50
200
A
2.0m
2.0m
2.0m
Figure 2.14a
B.

Expert Solution

This question has been solved!

Explore an expertly crafted, step-by-step solution for a thorough understanding of key concepts.

SEE SOLUTION Check out a sample Q&A here

Step 1

Step 2

Step 3

Step 4

Step by step

Solved in 4 steps with 4 images

SEE SOLUTION Check out a sample Q&A here

Knowledge Booster

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.

Similar questions

05. Consider the deformable pin-jointed truss with loading, geometry and section properties as shown in the Figure Q5. Given that E=2x10"N/m, A=10mm, L=Im and P-lkN. The horizontal displacement of Joint C (in mm, up to one decimal place) is „JointC P 2AE 7. AE AE Figure 05
show step by step solution
Current Attempt in Progress The cantilever beam consists of a rectangular structural steel tube shape [E = 29,000 ksi; = 1990 in."). For the loading shown, determine: (a) the beam deflection at point A. (b) the beam deflection at point B. Assume MA= 250 kip-ft, P= 14 kips, LAB = 4.1 ft, LBc = 6.2 ft. MA LAB LBC Answer: in. (a) VA- in. (b) VB - 4. Submi Attempts: 0 of 1 used Save for Later
A 30mm diameter bar is 1.25 m long. When the bar is simply supported at its ends in a horizontal position and is loaded with a concentrated load of 370 N at mid span, the central deflection was found to be 9.50 mm. In the second case, the bar is placed vertically and loaded axiallyThe buckling stress (in N/ mm²) of the vertical bar is
Q2/ For the two cases shown in Fig.2 (EI is constant) and by using unit load method, compare between the two cases according to the maximum deflection and show whom is the best loading that you think P= W*L 5 Marks Figure (2 B Case (1) Case (2)
Consider the timber beam shown below. The beam is made out of southern yellow pine, with an allowable bending stress of ?all= 2700 psi. The modulus of elasticity is E = 2,400 ksi. The maximum allowable deflection in the beam is 0.25 inches. A 1.5 kip/ft 6 ft 4 in. h B (a) What are the boundary conditions for this beam? (b) Determine the equation for the moment diagram using statics. (c) Determine the depth of the beam necessary to meet the allowable bending stress requirement.
Note: Here Data Is Different Than Previous Problem.
Please solve this question queckly
A steel beam is 24 inches tall, has a length, L, of 32ft, and has a yield stress of 36ksi. The simply supported beam supports a single load, P, of 17 kips at its midspan. If the theoretical maximum deflection of this beam is -(PL^3)/(48EI), determine the required moment of inertia such that the actual deflection of the beam will not exceed a value of L/360, and the actual stress will have a factor safety of 1.5 with respect to yielding.
Higdon
Aluminum [E = 72 GPa] member ABC supports a load of 31 kN, as shown in the figure. Determine (a) the value of load P such that the deflection of joint C is zero. (b) the corresponding deflection of joint B (positive if B moves up and negative if down). 1.0 m 1.3 m 31 KN C 34-mm diameter B 52-mm diameter