Figure 2a shows a uniform beam subject to a linearly distributed load. The equation for the resulting elastic (-x3 + 2L²×³ – L*x). (see Figure 2b) The following parameters are given for your Wo curve is y = - computation: L = 600 cm, E = 50000 kN/cm², I = 30000 cm“, and wo = 2.5 kN/cm. Use bisection method to determine the point of maximum deflection. 120EIL Wo -L· (a) (x = L, y = 0) (x = 0, y = 0) %3D (Б) Figure 2

Figure 2a shows a uniform beam subject to a linearly distributed load. The equation for the resulting elastic (-x3 + 2L²×³ – L*x). (see Figure 2b) The following parameters are given for your Wo curve is y = - computation: L = 600 cm, E = 50000 kN/cm², I = 30000 cm“, and wo = 2.5 kN/cm. Use bisection method to determine the point of maximum deflection. 120EIL Wo -L· (a) (x = L, y = 0) (x = 0, y = 0) %3D (Б) Figure 2

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: A rigid beam is being supported by three suspender bars made of bronze and loaded as shown in the…

Q: A sandwich beam having steel faces enclosinga plastic core is subjected to a bending momentM = 5 kN…

A: Given:- M = 5 kN . m. Es = 200 GPa. hp =140 mm, and Ep = 800 MPa. h =146 mm andb =175 mm. To find:-…

Q: The horizontal top of a concrete column is subjected to the system of forces shown. Represent the…

A: Sign convection Along axis direction = positive Along opposite direction = negative - Along x…

Q: Consider the beam in the figure below. Take P = 20 kN (Figure 1) Figure 60 kN-m A -2 m-1 m-1 m- -2m-…

A: A beam,Free body diagram of given beam:-

Q: A saw-tooth loading is applied as shown in the figure. The flexural stiffness (EI) of the beam is…

A: Given a propped cantilever beam carrying UVL loading. Required- To calculate support reactions.

Q: 3. Determine the strain energy of the beam shown in the figure below. The cross-section of the beam…

Q: saw-tooth loading is applied as shown in the figure. The flexural tiffness (EI) of the beam is 1×10³…

A: Given- A propped cantilever beam carrying UVL loading. Required- To calculate support Reactions of a…

Q: Consider the stress element as shown in figure. Determine the total distortion energy stored in 1 m…

A: For given state of stress,Young’s modulus of elasticity as E= 2 × 105 MPaPoisson’s ratio 0.3.

Q: Examine the 2D frame shown to the right. Solve the problem with the following set of properties: E =…

Q: normal strain in bar (2) is measured as –3,300 um/m. Use the dimensions L1 = 1,600 mm, L2 = 1,200…

A: According to given data The data given is question is different from the figure ,I am considering…

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

Figure 2a shows a uniform beam subject to a linearly distributed load. The equation for the resulting elastic
(-x3 + 2L²×³ – L*x). (see Figure 2b) The following parameters are given for your
Wo
curve is y = -
computation: L = 600 cm, E = 50000 kN/cm², I = 30000 cm“, and wo = 2.5 kN/cm. Use bisection method to
determine the point of maximum deflection.
120EIL
Wo
-L·
(a)
(x = L, y = 0)
(x = 0, y = 0)
%3D
(Б)
Figure 2

Expert Solution

This question has been solved!

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

This is a popular solution!

SEE SOLUTION Check out a sample Q&A here

Step 1

Step 2

Step 3

Step 4

Trending now

This is a popular solution!

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

Kindly answer the entire question(Q3) in the image given below. For your information, the unknown,w is given as 2. w=2
Consider the continuous beam as shown in figure below: RA 9,- 2 6 (m) R₂ What will be the magnitude of slope at B? H₂ 6 (m) Re
Problem #2 The bar shown below has uniform cross section and material properties throughout. In addition to the loads shown, the bar experiences a uniform temperature change of AT = 75.4 °F. Given the x displacement at A is equal to -0.2044 inches determine the magnitude of the external load P. Report your answer in kips to 2 decimal places. D 7.5 ft C 1.7P 4.5 ft B 2.3P 2.5 ft A 3.1P E 29,000 ksi a = 6.5 x 10-6 1/°F A = 0.1 in2
Q .A beam has a force of 25kN through the shear centre. For the system: a) determine the second moment of area about the x - x plane and b) determine the shear stress distribution along the y - y plane for positions A to F, c) plot the shear stress distribution on a suitable graph, labelling the principal values cross-section as shown in Figure Q. The beam is subjected to a vertical shearing Centre of Gravity X y 30 mm 180 mm y A B -C.-. -E- 10mm x 5mm Figure Q: Beam cross-section 30 mm 10 mm
Good comment will be given. Write the complete solutions and FBD legibly. Solve in 2 decimal places.
A cube of side 100 mm is subjected to an axial compressive load of 200 kN. Its lateral strain is prevented by applying uniform pressure but only one fourth of lateral strain could be prevented, then which of the following statements is/are correct? Assume E = 200 MPa and μ = 0.3. A The decrease in length in direction of load after applying pressure is 9.358 x 10-3 mm. B The uniform pressure applied has a value of 8.57 N/mm². C The uniform pressure applied has a value of 2.14 N/mm². D The increase in length in lateral direction after applying pressure is 2.25 x 10-³ mm.
Please answer the question in the picture 1.1 , and make sure you do the right work.
A simply supported beam is subject to a downwards uniform distributed load, w, as shown below. B A uniform distributed load, w L1 L2 The cross-section of the beam is constant with second moment of area I = 3750 mm², and Young's elastic modulus is E = 200 GPa. The distributed load has magnitude w = 220 N/m. If Point B is distance L₁ (Point C), calculate: the downwards vertical deflection at Point B: C C 435 mm from the left end (Point A) and distance L2 = 385 mm from the right end Round your answer to 3 significant figures. X [Units: mm]
In the figure below, the beam is cantilevered from the wall. The connection of the beam to the wall can be considered a general interaction. The beam has a uniform density, so it will be subject to a weight force applied mid-way between points A and B. length from point A to point B =10.0 meters; weight applied at point B = 1.00 kN; beam weight = 0.500 kN Beam embeded in cwalla cautilever B A What is the magnitude and direction (relative to the x-y coordinate system shown in the upper left portion of the figure) of the horizontal and vertical components of the wall support? horizontal = 0 N, vertical = 1.50 kN O horizontal = 1.50 kN, vertical = 0N O horizonatl = O N, vertical = 1.00 kN O horizontal = ON, verttical = 2.00 kN
Two identical loads distributed over circular areas are applied on an elastic two-layer system, as shown in the figure below. D E = 150,000 psi v = 0.5 h E = 30,000 psi v = 0.5 D/2 the dimensions and the magnitude of the surface stresses are: r= 6.5 in D= 16.25 in g = 75 psi h = 6.5 in Determine: 1. The total vertical deflection at point A 2. The total vertical deflection at point B 3. The total vertical deflection at point C
Q2) The figure shows a cantilever consisting of steel channel size 127 mm×64 mm. Using superposition, find the deflection at B and the maximum stress in the beam. Take the magnitude of force (F) to be 1.3 kN, L = 3 m, and a = 1.8 m. Calculate the deflection at point B in (mm). Use E= 207 GPa. F 1 kN/m B A