Please solve the problem in the picture Problem 3Draw (a) the shear and bending-moment diagrams for the beam and loading shown, (b) determine themaximum normal stress due to bending, and (c) sketch the normal stress distribution on the section.Sectional Area Ix ly Sx Sy(cm) (cm) (cm³) (cm³)80 kN/mHinge160 kND(cm²)EH76.112860 1829 849 180.8W310 x 60-2.4 m0.6 m1.5 m1.5 mRecall that if you have a hinge in thebeam, you have to break the beam atthe hinge and draw the FBDs for all theparts (see the example I solved in class).AyThis will allow you to find externalExBx' Bx'Bx" Bx"By'By' By"By"CyEyreaction forces at the supports and internal reaction forces at the hinge.Mmax = 84 kNm, σmax = 98.9 MPa

Answered: Problem 3 Draw (a) the shear and…

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

See similar textbooks

Similar questions

The cantilever beam in the figure is the result of joining three parts with nails. has been created. As each nail carries 90ON cutting force a) Determine the nail spacing. b) Draw the shear stress distribution in the most stressed section. 12kN 8kN B 3cm I 30cm 1.2m 1.2m 20cm Зст 3cm
%3D QUESTION 2. An oblique bending moment of M = 5 kN.m is applied on the cross-section of an aluminum beam as shown in the figure. (a) Calculate the maximum values of compressive and tensile normal stresses on the crss section. (b) Define the orientation of the neutral axis and draw on the cross-sectionç. M = 5 kN.m 30° 10 mm 40 mm 10 mm A-40 mm--r: 30 mm 30 mm 10 mm 10 mm
the largest axial P force that the given riveted joint can safely carry.calculate. Rivet diameter 32mm and plate width 310mm. Shear stress of the rivet1400 kg/cm2, crush safety stress of rivet 2800 kg/cm2and the platetensile safety tension 1400 kg/cm2will be taken. t1=20mm t2=37mm
13. A block 100mm x 100mm base and 10mm height. What will the direct shear stress in the element when a tangential force of 10kN is applied to the upper edge to a displacement 1mm relative to lower face?
0.200 mm S R 250 mm 0.380 mm P 500 mm A thin rectangular plate is uniformly deformed as shown. Determine the in-plane shearing strain at point P rad 0.00156 rad 0.00076 rad 0.00080 rad 0.00257 rad 0.00128
Problem 7: The rectangular plate is deformed into the shape shown by the dashed lines. Determine the average normal strain along diagonal AC, and the average shear strain at corner A relative to the x, y axes. (8 pts) 6 mm -400 mm 2 mm mm fom 300 mm 2 mm A B 400 mm -3 mm
3) The plate shown is fixed connected along AB and held in the horizontal guides at its top and bottom, AD and BC. If its right side CD is given a uniform horizontal displacement of 4 mm, determine (a) the average normal strain along the diagonal AC, and (b) the shear strain at E relative to the x, y axes y. i= 340 mm j= 479 mm D k = 170 mm A k E j k B i 4тm
2. The lengths LAB = LBC = 200 mm and LCD = 240 mm. The diameter of parts AB and CD of the bar is 25 mm and the diameter of part BC is 50 mm. The shear modulus of the material is G = 80 GPa. What value of the %3D torque T would cause the angle of twist of the right end of the bar relative to the wall to be zero? 4 kN-m A 8 kN-m LAB B T LBC.
Consider the element in with Txy = 30 MPa. 80 MPa Part A 01, 02 Determine the principal stresses. Enter your answers in megapascals to three significant figures separated by a comma. = T vec Submit VE ΑΣΦ | 41 Txy Request Answer
A:Y 211O 2_531929016114... -> A rod is composed of an aluminum section rigidly attached between steel and bronze sections, as shown in Figure below. Axial loads are applied at the positions indicated. If P = 11 KN and the cross sectional area of each rod is 312.5 mm, determine the stress in each section. 4P Steel Bronze |Aluminum 609.6 mm 914.4 mm 762 mm
Detemine the principal stress acting at point B, which is located just on the web, below the horizontal segment on the cross section Show the results on a properly oriented element located at this point. Although it is not very accurate, use the shear formula to calculate the shear stress. -AO mm- 300 mm 150 mm 12 mm 130 mim 15 mm 6 kN
beam.pdf For the beam shown below, draw bending stress distribution along the depth of beam at critical section. 50 kN 120 20 3 m 3 m

SEE MORE QUESTIONS

Recommended textbooks for you

Structural Analysis

Civil Engineering

ISBN:

9781337630931

Author:

KASSIMALI, Aslam.

Publisher:

Cengage,

Structural Analysis (10th Edition)

Civil Engineering

ISBN:

9780134610672

Author:

Russell C. Hibbeler

Publisher:

PEARSON

Principles of Foundation Engineering (MindTap Cou…

Civil Engineering

ISBN:

9781337705028

Author:

Braja M. Das, Nagaratnam Sivakugan

Publisher:

Cengage Learning

Structural Analysis

Civil Engineering

ISBN:

9781337630931

Author:

KASSIMALI, Aslam.

Publisher:

Cengage,

Structural Analysis (10th Edition)

Civil Engineering

ISBN:

9780134610672

Author:

Russell C. Hibbeler

Publisher:

PEARSON

Principles of Foundation Engineering (MindTap Cou…

Civil Engineering

ISBN:

9781337705028

Author:

Braja M. Das, Nagaratnam Sivakugan

Publisher:

Cengage Learning

Fundamentals of Structural Analysis

Civil Engineering

ISBN:

9780073398006

Author:

Kenneth M. Leet Emeritus, Chia-Ming Uang, Joel Lanning

Publisher:

McGraw-Hill Education

Sustainable Energy

Civil Engineering

ISBN:

9781337551663

Author:

DUNLAP, Richard A.

Publisher:

Cengage,

Traffic and Highway Engineering

Civil Engineering

ISBN:

9781305156241

Author:

Garber, Nicholas J.

Publisher:

Cengage Learning

SEE MORE TEXTBOOKS