Answered: Use the unit load method to calculate…

Use the unit load method to calculate the vertical displacements at the quarter and mid-span points in the beam shown in Fig. P.15.8. Ans. 57wL'16144EI, 5wL*1384EI. (both downwards)

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: P02: The beam of Fig. 2 has a simple span of 20 ft and supports a dead load including its own weight…

A: span= 20 ft DL= 1 klfLL = 0.7 klff'c = 3000 psi To find- 1) Instantaneous deflection for D+L2)…

Q: B1 a) b) c) The simply supported beam in Fig QB1a is made by gluing two pieces of wood of…

A: Given: To find: a) Support reactions, Bending moment diagram, and Shear force diagram b) Moment of…

Q: 4.1) For the beam shown, derive the expressions for V and M, and draw the shear force and bending…

A: Step 1: Step 2: Hope this helps!

Q: A structural designer wishes to locate the roller support B such that the beam AD) in Fig. P6.4-13…

Q: 21-30. A system of cords knotted together at A and B support the weights shown in Fig P-311. Compute…

A: This problem is related to Mechanics from Civil Engineering. In this problem given about two weight…

Q: P16.10 Vertical Both reactions and the shearing force and bending moment at section 1-1. (Ans: load…

Q: 19. AT-section of a beam, as shown in Fig. 5.44, is subjected to a vertical shear force of 100 kN.…

Q: 1 Which of the following gives the shear as function of 'x' of segment BC on the beam shown. 'x'…

Q: loading scenario: uniform dead load of 1 klf, a moving uni- ber BC of the truss in Problem 16.49…

Q: 54.9. Bodies A and B are joined by a cord parallel to the inclined plane shown in Fig. P-5-4.9.…

Q: Compute the forces in bars AB, AC, DF, and DE of the scissors truss shown in Fig. P-433

A: Moment about J=0ΣMJ=0RA x 60=12x10+12x20+12x30+12x40+12x50RA=30 KRJ=30 K

Q: Prob. 2.3-7. For small loads, P, the rotation of "rigid" beam AF in Fig. P2.3-7 is controlled by the…

Q: Prob. 1.4-13. For the overhanging beam shown in Fig. P1.4-13: (a) determine expressions for the…

Q: 200 kN-m QB -5 m M = 6(x-5)^2 - 70x + 450 M = -6(x-5)^2 - 70x - 450 -10 m

Q: 6.145 The pliers shown are used to grip a 0.3-in-diameter rod. Knowing that two 60-lb forces are…

Q: that two 60-lb forces are applied to the magnitude of the forces exerted on the by the pin at A on…

Q: Design the beam shown in Fig.3.24. The beam is subjected to a positive bending moment of 540 kN-m,…

A: The values and diagram given in the question are as follows: Bending moment(M)=540 kN-m Materials…

Q: Analyze the beam of Problem 11.1, which is subjected to the indicated loads if support B settles 2.0…

Question

Use the unit load method to calculate the vertical displacements at the quarter and mid-span points
in the beam shown in Fig. P.15.8.
Ans. 57wL*16144EI, 5wL*1384EI. (both downwards)

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

Step 5

Step 6

Step 7

Step 8

Step 9

Step 10

Trending now

This is a popular solution!

Step by step

Solved in 10 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

75 N E 720 В D12.5 A 4.91 Determine the clamping force at A due to the 75-N horizontal force applied to the handle at E. 90 +165→l+ -360 Dimensions in mm Fig. P4.91
Use the unit load method to calculate the deflection at the free end of the cantilever beam ABC shown in Fig. P.15.10. Ans. 3 WL³18EI. (downwards)
Q.No 6. a) Determine the horizontal deflection at joint E of the truss shown in Fig. due to a temperature increase of 50C in members AC and CE. Use the method of virtual work. b) Determine the horizontal deflection at joint E of the truss shown in Fig. if member BC is 18 mm too long and member CE is 15mm too short. Use the method of virtual work. 4m D 4m 3m-
Prob. 1.4-13. For the overhanging beam shown in Fig. P1.4-13, determine: (a) expressions for the internal resultants V,(x) and M,(x) in interval AB (0
Prob. 1.4-13. For the overhanging beam shown in Fig. P1.4-13, determine: (a) expressions for the internal resultants V¡(x) and M1(x) in interval AB (0 < x < 6 in.), and (b) the internal resultants Vp and Mp at section D, midway between the two supports. 40 lb/in. A |c B D 6 in. 3 in. -3 in. P1.4-13
please answer asap
3. The vertical load carried by the simply supported beam in Fig. 3 increases consistently from zero at the left end to a maximum of 8000 N/m at the right end. Create diagrams for the bending moment and shearing force. R₁ (a) 0 5600 N mum 8000 N/m R₂ (1905xxx! R₁ 2.8 m 'T 8000 N/m mmm. 11 200 N 16800 N 1.4 m
Each of the three beams shown in Fig.Q3 has been provided with supports imposing more constraints on movement than the minimum necessary to achieve static equilibrium. The built in supports prevent all lateral movements and rotations, but do not resist longitudinal movement. Beam (a) has a simple support at the right hand end which does not move vertically. The right hand support for beam (b) prevents a change of slope but does not exert a vertical force. Each beam is made from titanium, for which Young's modulus is 106GPa and the yield stress in 780MPa. The cross-section is square and tubular, having outside dimensions of 12mm and a wall thickness of 1.5mm. Loading. is parallel to the sides and acts through the centroid. For each beam: i. calculate the support forces and moments ii. determine an expression for the bending moment at every point in the beam and draw the bending moment diagram iii. determine an expression for the deflection curve; draw the curve and state the maximum…
Each of the three beams shown in Fig.Q3 has been provided with supports imposing more constraints. on movement than the minimum necessary to achieve static equilibrium. The built in supports prevent all lateral movements and rotations, but do not resist longitudinal movement. Beam (a) has a simple support at the right hand end which does not move vertically. The right hand support for beam (b) prevents a change of slope but does not exert a vertical force. Each beam is made from titanium, for which Young's modulus is 106GPa and the yield stress in 780MPa. The cross-section is square and tubular, having outside dimensions of 12mm and a wall thickness of 1.5mm. Loading is parallel to the sides and acts through the centroid. For each beam: i. calculate the support forces and moments ii. determine an expression for the bending moment at every point in the beam and draw the bending moment diagram iii. determine an expression for the deflection curve; draw the curve and state the maximum…
Problem 813 Determine the moment over the support R₂ of the beam shown in Fig. P-813. R₁ 4m 1400 N/m R₂ 900 N -1m-1m- Figure P-813 800 N/m 2 m R3
answer with fbd please
Problem 2: Find the smallest diameter bolt that can be used in the clevis shown in Fig. 1-11b if P = 500 kN. The shearing strength of the bolt is 320 MPa. P.