The mounting arm shown in the figure below is to be made of machined AISI 1050 CD steel and is subjected to the aial force 120 An cyces repeatedy from tension to compression, and the completely reversitie cycdtorsional moment of T25AN Assume the component is operating at room temperature of 0 and the material has sos refiablity factor. Aso asume K138 and-13256 mm Dr=3 mm%3D50 mm D1. Identity the critical location(s) of stress and show it clearly in a diagram2 Identify cleary, all the components of stresses (at the critical point) that will be calculated (by drawing and clearly showing the XYZ axes) and show it in a matrix form Show which components of stresses will have a vazero or non-zero3. Calculate the principar stresses and principal directions. Show the principal stresses dearty in a stress element with respect to original XYZ coordinate system4. Clearly show the calculations for all the 6 Marin factors (Use only the formula sheet provided in the beginning of the test) and calculate the endurance limit, s,5 Calculate the amplitude and mean value of axial force and coresponding stress valuesa. Calculate the ampitude and mean value of torque and corresponding stress values.7. Calculate the fatigue factor of satety upto 4 digits after decimal point using Gerber criterion8 Calculate the yield factor of safety, upto 4 digits after decimal point0. Does the component fail or does not fal?10. Cauloulate the numer of cycles to failure

Answered: Image /qna-images/answer/746a13a1-2e2b-45ea-8be7-1677f8917b7d.jpg

ions. Show the principal stresses dearty in a stress element fors (Use only the formula sheet provided in the beginni ce and comesponding stress values and coresponding stress values s after decimal pont using Gerber criterion after decimal point

ions. Show the principal stresses dearty in a stress element fors (Use only the formula sheet provided in the beginni ce and comesponding stress values and coresponding stress values s after decimal pont using Gerber criterion after decimal point

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

This is my ID :201903062
Determine the state of stress of a beam at the point shown in Figure 2 to represent: a) the principal stresses; b) the maximum in-plane shear stress and the associated average normal stress. c) For each of the two cases mentioned in (a) and (b), determine the corresponding orientation of the element with respect to the original element shown and sketch the results relative to the longitudinal axis of the beam. Please show the full working to provide sufficient information for the sketching to be complete. 15MPa Figure 2 20° 50MPa
Calculate the stress perpendicular to the inclined plane AB. Report your answer as a positive number.Answer: σn= Enter your answer in accordance to the question statement ksi.
Engineering and true
The state of stress shown to the left was produced by a combination of loadings on a body that is not shown. Determine the following via Mohr's circle: A) Draw Mohr's Circle for the x-y plane. B) Determine the principal stresses - All 3. C) Sketch a properly oriented differential element showing the principal stresses in the x-y plane. D) Determine the magnitude of the maximum shear stress in the x-y plane. E) Sketch a properly oriented differential element showing the maximum shear stress state in the x-y plane. F) Determine the magnitude of the absolute maximum shear stress (and include the two out of plane circles on your original figure). Use the following values for the magnitudes of the stresses: x = 0₂ Txy Ox X X 10 ksi, σy = 4 ksi, σ₂ = 3 ksi, Txy = 4 ksi
This my id 201901782
Learning Goal: To determine the average normal strain and average shear strain in a known material based on a given load and geometry. A flat plate ABCD distorts into the dashed shape ABCD shown after a load is applied with a (AC) v = Y Part A- Average normal strain along AC Determine the average normal strain (AC) avg along AC after the load has been applied. Express the average normal strain in millimeters per millimeter to three significant figures. View Available Hint(s) [ΕΙ ΑΣΦ 212 Yay= D Part B - Average shear strain at A Submit It vec ^ d C Yzy = Determine the average shear strain Yay at A relative to the x and y axes. Express the average shear strain in radians to three significant figures. ► View Available Hint(s) 15. ΑΣΦ ? ↓↑ vec Part C Average shear strain at point C 163.0 mm, b= 49.0 mm, 9 - 11.0 mm. f-18.0 mm, and e = 14.0 mm 195| ΑΣΦ | 41 mm/mm vec wwwww. Determine the average shear strain Yay at point C relative to the x and y axes after deformation. Express the average…
Rank the normal stress in each section of the bar. Rank the values of normal stress from largest (largest tensile stress) to smallest (largest compressive stress). Use AB for segment AB, BC for segment BC, and CD for segment CD.
a. What is the stress in MPa at point B? b. What type of stress "at point B"
In the following Figure using given material properties.a) Determine the internal forces and stresses at both parts after 110 oC temperature increase.b) Determine the new position of B with respect to the point A.
Use Mohr's Circle to determine the maximum shear stress on the element, also using Mohr's Circle determine the maximum normal stress on the element.
Need only handwritten solution only (not typed one).