different cross section designs (WWF and reactangle), a) Calculate the max tensile stress and shear stress for each design. For the WWF beam, you may calcualte the average shear stress by considering the web contribution only. b) Sketch the distribution of normal stress and shear stress along the height of each cross section. c) Compare the max stress and the cross sectional area of each design and discuss which design is more efficient. 20 mm: 20 mm: B 20 mm C - 150 mm 150 mm 104mm -250 mm- The moment of inertia for the WWF section is I=310.3 x 106 mm². 320mm

different cross section designs (WWF and reactangle), a) Calculate the max tensile stress and shear stress for each design. For the WWF beam, you may calcualte the average shear stress by considering the web contribution only. b) Sketch the distribution of normal stress and shear stress along the height of each cross section. c) Compare the max stress and the cross sectional area of each design and discuss which design is more efficient. 20 mm: 20 mm: B 20 mm C - 150 mm 150 mm 104mm -250 mm- The moment of inertia for the WWF section is I=310.3 x 106 mm². 320mm

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

In the following table, a part of a project, for which the time period for each activity is specified, find the time required to complete the project using the network diagram by Act. on arrows. Activity A B D G H I Time Followed by Preceded by B.C 23573625 G.F D.F E I I H I A A C B.C DBG H.E.F
A small aluminum alloy [E= 77 GPa] tee shape is used as a simply supported beam as shown. For this beam, a = 160 mm. The cross- sectional dimensions of the tee shape are b= 22 mm, d = 33 mm, and t= 4 mm. After loads are applied to the beam at B, C, and D, a compressive normal strain of 410 uɛ is measured from a strain gage located at c = 10 mm below the topmost edge of the tee stem at section 1-1. What is the applied load P? %3D %3D %3D 3P Strain gage E Answer:
i need the answer quickly
what is the modulus elasticity of 20 mm rod when a 250 MPa stress is exerted the total elastic deformation measured is 0.2mm
The state of plane stress shown occurs at a critical point of a steel machine component. As a result of several tensile tests, it has been found that the tensile yield strength is o, = 250 MPa for the grade of steel used. Determine the factor of safety with respect to yield using (a) the maximum shearing stress criterion, and (b) the maximum distortion energy criterion. ↑y 40 40 MPa 80 MPa 25 MPa ➜X
Determine the maximum tensile stress in the beam shown.
asap please thank you
PROBLEM 1) An aluminum bar carries the axial loads at the positions shown. If E=70GPA, compute the total deformation of the bar. Assume that the bar is suitably braced to prevent buckling. 0.4m D 10KN 6) What is the deformation &c in mm? 0.8m 0.4m B 5KN 0.6m 20KN A=800 mm? A=1,200 mm²
Find the stress produced in rod due to tensile load of 2.02 N whose cross section area is 2 mm2
Read the question carefully and give me both right solutions with clear explanation. Don't copy from other websites solution