soru 1 c) Draw the normal stress distribution that will occur in b)) Draw the shear stress distribution that will occur in the cross section at point C. a) Draw Shear Force and Moment Diagrams. the section just to the left of point c. AND SHOW THE LARGEST AND SHOW THE LARGEST SLIP STRESS VALUE BY STRESS VALUES BY CALCULATING. CALCULATING.. P1 (kN) Kiriş kesiti A h (cm) L1 (m) L2 (m) b (cm) P1 (kN) L1 (m) L2 (m) b (cm) h (cm) 48 1.0 2.0 18 28

soru 1 c) Draw the normal stress distribution that will occur in b)) Draw the shear stress distribution that will occur in the cross section at point C. a) Draw Shear Force and Moment Diagrams. the section just to the left of point c. AND SHOW THE LARGEST AND SHOW THE LARGEST SLIP STRESS VALUE BY STRESS VALUES BY CALCULATING. CALCULATING.. P1 (kN) Kiriş kesiti A h (cm) L1 (m) L2 (m) b (cm) P1 (kN) L1 (m) L2 (m) b (cm) h (cm) 48 1.0 2.0 18 28

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

Consider a point in a structural memberthat issubjected to planestress. Normal and shear stress magnitudes acting on horizontal and vertical planes at the point are S-45 MPa,S,-67 MPa, andS-21MP., (a) Draw Mohr's circle for this state of stress. (b) Determine the principal stresses and the maximum in-planeshear stress acting at the point. (c) Show these stresses on an appropriate sketch (e.g. see Fig. 12.15 or Fig 12.16). (d) Determine the absolute maximum shear stress at thepoint Sy Determine the principal stresses and the maximum in-plane shear stress acting at the point. Say Answer: MPa MPa MPa Tomaxin plane
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
If Øxx = 110 MPa, Oyy = - 86 MPa, ozz = 55 MPa. Txy = 60 MPa, and allþther components are zero. Determine the principal stresses and the direction cosines of the principal axis. Also find the octahedral normal and shear stress components. Q.4:
The stresses at a point are measured as shown. Using Mohr's circle determine the stresses with respect to x' - y' axes. Also, determine the maximum possible shear stress at this point. „3.5 MPa 18° '4.4 MPa
need help with assignment thankss....(especially the mohrs circle part for the graph) x=4, y=4, A=13
Consider a point in a structural member that is subjected to plane stress. Normal and shear stress magnitudes acting on horizontal and vertical planes at the point are Sy-17 MPa, S, - 60 MPa, and Swy- 29 MPa. (a) Draw Mohr's circle for this state of stress. (b) Determine the principal stresses (ơp > op2) and the maximum in-plane shear stress Tmax acting at the point. (c) Find the smallest rotation angle 0, (counterclockwise is positive, clockwise is negative) that will rotate to principal directions. Then show these stresses in an appropriate sketch (e.g, see Figure 12.15 or Figure 12.16) Say Answers: MPa. Opl = MPa. MPa. Tmax = 0, =
Stress in shaft due to Bending Load and Torsion. A shaft has a diameter of 4 cm. The cutting section shows in the figure is subjected to a bending moment of 2 kN-m and a torque of 2.5 kN-m. Determine: 1. The critical point of the section 2. The stress state of the critical point 3. The principal stresses and its orientation Using Morh’r and Draw Stress element transformation
len 2
2.18. The stress at a point is defined by the components Oxr = 85 MPa, Oyy= 320 MPa, oz= 100 MPa, Ory =-40 MPa, ơ =50 MPa, ơzx=-20 MPa. Find the three principal stresses, sketch the three Mohr's circles and hence determine the magnitude of the maximum shear stress. yz
Please solve the problem in the question, Make sure you show all of your work please
Please show intermediate steps including free body diagrams, equations used, problem setup etc. so that your approach can be followed.
Your answer is partially correct. Determine the absolute maximum shear stress for each of the following plane stress states for which the principal stresses are given. (a) op1 = 2780 psi, o,2 = -2440 psi, op3 = 0 (b) Op1 = 58 MPa, Op2 = 35 MPa, Op3 = 0 Answer: (a) Tabs max psi 1390 (b) Tabs max MPa 29