A T-shape beam is subjected to a vertical shear force of V = 30 kN. The beams centroid is located 211.1 mm above thebottom surface of the beam, and the moment of inertia is l₂ = 48.7 x 106mm4.[b = 178 mm, h = 300 mm, t₁ = 12.7, tw = 9]bhtwDetermine the shear stress in the flange at the intersection of the flange and the web.6.96 MPa7.6 MPa2.94 MPa4.3 MPa6.09 MPa A T-shape beam is subjected to a vertical shear force of V = 30 kN. The beams centroid is located 211.1 mm above thebottom surface of the beam, and the moment of inertia is l₂ = 48.7 x 106mm4.[b = 178 mm, h = 300 mm, t₁ = 12.7, tw = 9]bhtwDetermine the maximum shear stress in the entire section.Answer:MPa

Answered: Image /qna-images/answer/eb65df7f-391a-47c0-9050-182f0c2b0dde.jpg

Answered: v tf MPa Pa MPa Pa h - tw the shear…

Engineering

Civil Engineering

v tf MPa Pa MPa Pa h - tw the shear stress in the flange at the intersection

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

%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 internal shear force V at a certain section of an aluminum beam is 40 kN. The beam's centroid is located 54.40 mm above the bottom surface of the beam, and the moment of inertia is l₂ = 398,300 mm4. Determine the shear stress at point H, which is located 30 mm above the bottom surface of the beam. 30 mm 75 mm y H 5 mm 5 mm 75 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.
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 cross section. (b) Define the orientation of the neutral axis and draw on the cross-sectionç. M = 5 kN.m 30° 10 mm 40 mm y 10 mm At-40 mm-- 30 гу 30 mm 10 mm 10 mm
Determine the maximum normal stress on a transverse plane in the straight portion of the structure shown below and clearly indicate where it occurs. The member is braced in the plane perpendicular to the plane of symmetry. Consider: (a) Section B-B shown below at the left (symmetric section). (b) Section B-B shown below (unsymmetric). 4 40 kN 750 mm 75 mm 50 mm 100 mm mm 09: Section B-B 100 mm A 150 mm 50 mm 30 mm 80 mm 20 mm 09 1200 mm Section B-B, part b
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
The structure shown is supported by a steel rod at B. Specifications of the steel rod L= 2m d=25 mm E=200 GPa Show complete solutions 1. Draw the shear force and bending moment diagrams. 2. Determine the stress in the steel rod at B 3. Determine the deflection at A
I need your help
Use the virtual work method to determine the deformation at joint B of the truss shown. 3 m A -2 m 100 KN B 50 kN -4 m- EA constant E = 70 GPa A = = 1,000 mm² C
1. Calculate the moment of inertia of the section in mm . 2. Calculate the location of the neutral axis from the bottom of the beam in mm. 3. Calculate the maximum moment in the beam in kN.m. 4. Calculate the flexural stress at a section 75mm from A and 40mm from the bottom of the beam in MPa. 5. Calculate the maximum compressive flexural stress of the beam in MPa. 6. Calculate the maximum tensile flexural stress of the beam in MPa. NOTE: Kindly answer all numbers with complete solution please. Needed ASAP.
This is a mechanics of deformable bodies problem