2. The simply supported beam below has the cross-sectional area shown.a.Draw the FBD (2 pts)b. Determine the absolute maximum bending stress in the beam (2 pts) Your Answer: --Determine the bending-stress at points A & C. (1 pts) Your Answer:&Plot the bending-stress distribution acting over the beam's cross section (1 pts)c. Determine the absolute maximum shear-stress in the beam (2 pts) Your Answer:Determine the shear-stress at points A & C. (1 pts) Your Answer:&Plot the shear-stress distribution acting over the beam's cross section (1 pts)A20 kN/m4 mDesignationmm x kg/mW150 x 14Areamm-1730OB4mm2 m15020 kNWebDepth thickness widthbymmmmCFlange4.32 100.0thickness"fmm5.5‒‒‒‒‒‒‒‒‒‒‒.HCX-X axisS10 mm 10³ mm³6.8491.2Armm62.9

The objective of the question is to analyze the stress distribution in a simply supported beam under…

Answered: 2. The simply supported beam below has…

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

See similar textbooks

Similar questions

A 20 ft long simply supported beam has 15-inch outside diameter with 1-inch-thick circular section. The beam carries 10 lb/ft uniformly distributed load from the right support to its middle span. Another 15 lb concentrated load applied downward in the left-end support. Determine the maximum bending stress (k-lb/ft2) of the simply supported beam.
A beam is supported and loaded as shown. In the section of the beam between 'A' and 'B', the equation for the resisting bending moment was determined as: M₁ = -6.5x²+50x. Determine the magnitude of maximum resisting bending moment (Mr,max) in the section. Note: Do NOT include units in your answer Answer: AA B
4. A cantilever beam 3 m long carries a concentrated load of 35 kN at its free end. The material is structural steel and the maximum bending stress is not to exceed 125 MPa. Determine the required diameter (mm) of the bar if it is circular.
. Determine the maximum bending stress in the beam with the circular cross-section. 400 lb B 200 lb/ft 2 in. |2 ft 5 ft- -4 ft - Figure 5.5.6
If the simply supported beam is subjected to the load shown below, determine the following: c- c - The internal bending moment acting on the cross-section through point C. d- d- The shear stress at section C.
Use the graphical method to construct the shear-force and bending-moment diagrams for the beam shown. Let a=4.0 ft, b=8.0 ft, c=4.0 ft, d=3.0 ft, w = 6.5 kips/ft and P = 45 kips. Construct the shear-force and bending-moment diagrams on paper and use the results to answer the questions in the subsequent parts of this GO exercise. a B a W B W C b d For this loading, calculate the reaction forces Ay and Ey acting on the beam. Positive values for the reactions are indicated by the directions of the red arrows shown on the free-body diagram below. (Note: Since Ax = 0, it has been omitted from the free-body diagram.) b C C P C D P Ľ E d E ·x Ey
This laboratory focusses on the bending of a simply-supported beam, as shown in the following schematic (Figure 1). W/2 Z a 6.4mm X W/2 23mm Figure 1 the loading scheme of a beam It can be shown that for this loading case, the bending moment for a ≤ x ≤ L-a is constant and equal to Wa/2. In this experiments, a = 350 mm and L = 835 mm. Loading the beam in this way, rather than loading the beam at just one point, has two main advantages: (i) it allows a strain gauge to be placed at the top of the beam and (ii) the constant bending moment area that it creates gives better strain gauge performance when stretched or compressed. 6.4mm W/2 8mm a 38.1mm W/2 indicates strain gauge 38.1mm Figure 2 the dimensions of the cross section of the beam and the position of the strain gauges
Determine the absolute maximum normal stress (in unit of MPa) in the beam with external loadings shown below. The beam has a uniform square cross-section with lateral size a = 0.2 m. Note: (1) the shear and moment diagrams can be calculated by either section method or graphical method; (2) there is a concentrated load at point A and a bending moment at point C. 20 kN w = 20 kN/m Mc = = 80 kN · m || В A¬Q C y 2 m 2 m 2 m
For the beam shown, calculate the magnitude of the bending stress (in psi) at the top of the beam on a section 1.84 feet to the right of B if P = 1317 lb, Q = 4548 lb, w = 1.5 in, L = 8.66 in, b = 4.03 in, and h = 1.67 in. Round off the final answer to two decimal places. ... P Q W D 2 ft 3 ft——3 ft— 2 ft Add your answer
The cross-sectional dimensions of a beam are shown. Assume b=3.625 in., tetw=0.1875 in. and d=4.125 in. (a) If the bending stress at point K is 2470 psi (T), determine the internal bending moment M, acting about the z centroidal axis of the beam. (b) Determine the bending stress oy at point H (positive if tension, negative if compression). K d H Answers: (a) M2 = i Ib-ft. (b) oH = i psi.
2. A 150 kip-ft (negative 150 kip-feet) moment is acting at the centroid of the cross section shown on the next page. Determine the bending stress-in psi - at a point that is located (a) at the top surface of the cross section. (b) 3 inches down from the top surface of the cross section. (c) 12 inches up from the bottom surface of the cross section. (d) 3 inches up from the bottom surface of the cross section. (e) at the bottom surface of the cross section. M
Consider an 8-m long simply supported T-beam with overhangs loaded as shown below. 200 mm w kN/m 50 mm 50 kN-m 50 kN-m 200 mm 2 m 4 m 2 m 50 mm 1. Determine the location of the neutral axis measured from the top of the beam and the moment of inertia (in mm4) of the section about its neutral axis. Draw the shear and bending moment diagrams. Annotate all relevant values and distances. Determine the magnitude of the maximum negative 2. moment. Determine the minimum allowable strength of the beam in tension and the minimum allowable strength of the beam in compression. 3. Determine the maximum allowable load, w (in kN/m), that can be applied pn the beam. 4. B.

SEE MORE QUESTIONS

Recommended textbooks for you

Elements Of Electromagnetics

Mechanical Engineering

ISBN:

9780190698614

Author:

Sadiku, Matthew N. O.

Publisher:

Oxford University Press

Mechanics of Materials (10th Edition)

Mechanical Engineering

ISBN:

9780134319650

Author:

Russell C. Hibbeler

Publisher:

PEARSON

Thermodynamics: An Engineering Approach

Mechanical Engineering

ISBN:

9781259822674

Author:

Yunus A. Cengel Dr., Michael A. Boles

Publisher:

McGraw-Hill Education

Elements Of Electromagnetics

Mechanical Engineering

ISBN:

9780190698614

Author:

Sadiku, Matthew N. O.

Publisher:

Oxford University Press

Mechanics of Materials (10th Edition)

Mechanical Engineering

ISBN:

9780134319650

Author:

Russell C. Hibbeler

Publisher:

PEARSON

Thermodynamics: An Engineering Approach

Mechanical Engineering

ISBN:

9781259822674

Author:

Yunus A. Cengel Dr., Michael A. Boles

Publisher:

McGraw-Hill Education

Control Systems Engineering

Mechanical Engineering

ISBN:

9781118170519

Author:

Norman S. Nise

Publisher:

WILEY

Mechanics of Materials (MindTap Course List)

Mechanical Engineering

ISBN:

9781337093347

Author:

Barry J. Goodno, James M. Gere

Publisher:

Cengage Learning

Engineering Mechanics: Statics

Mechanical Engineering

ISBN:

9781118807330

Author:

James L. Meriam, L. G. Kraige, J. N. Bolton

Publisher:

WILEY

SEE MORE TEXTBOOKS