A2 in1-in dia.Bin1½ inFy 2-in dia.6 in5 inFor the cantilevered handle shown, the force Fy applied at D is 1000 lbs in the y-direction. Please determine:Make sure you INCLUDE shear stresses due to bending!1. The loads at point C (identify magnitudes and directions of forces and/or torques and/or moments atpoint C).2. The loads at point B (identify magnitudes and directions of forces and/or torques and/or moments atpoint B).3. Using the Distortion Energy Theory (DET), determine the STRESS on an element A (see insert).4. Using the Maximum Shear Stress Theory (MST), determine the STRESS on an element B (seeinsert).

2. Loads at Point BMagnitudes and Directions of Forces and/or Moments at Point B:To balance the…

Answered: A 2 in 1-in dia. B in 1½ in Fy 2-in…

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

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Given the beam and the external loading shown below, if L = 15 m, w1 = 510 N/m and w2 = 1,600 N/m, calculate: • the magnitude and location of the equivalent resultant force (a single equivalent force, for the whole loading block, NOT two equivalent forces from dividing into rectangular and triangular stress blocks). • the reactions at the beam supports. W2 w, A L Resultant force Fr = 单位 (tolerance 1 N, magnitude only) Location xbar = 单位 (tolerance 0.1 m, measured from A) Reactions: Ay = 数字单位 (tolerance 1 N, observe up positive sign convention) MA= 数字单位 (tolerance 10 N*m, observe anti-clockwise positive sign convention)
Below Figure shows the section of an angle purlin. A bending moment of 60 5 kN.m is applied to the purlin in a plane at an angle of 30 deg to the vertical y axis. If the sense of the bending moment is such that both its components Mx and My produce tension in the positive xy quadrant, calculate the maximum direct stress in the purlin, stating clearly the point at which it acts. * 100 mm BỊ 10mm 30° C ID 10mm 57 MPa. 89 MPa. Non Above 72 MPa. 125mm
0.15m 0.75m 0.60m H 1.00m M 1.50m Figure 1: Representation of the frame system T 0.60m Figure 2: Detailing of support G 30mm 20mm
Problem 1 Please choose the correct answer and also write down your solution. (1) The section supports an upward internal shear force and a clockwise internal torque. Where does the absolute maximum shear stress occur? a. Point A b. Point B c. Point C d. Point D (2) The internal force and moment of the section have been determined as F = 100î + 300k (N) and M = 50î + 40j (N - m). Where does the absolute maximum normal stress occur? a. Point A b. Point B c. Point C d. Point D
Question 2) A force of magnitude F=28 kN, which makes an angle of θ=35 ° with the horizontal in the xz plane from point B, and a moment of magnitude M=18 kN.m from point C in the z direction acts on the arm in the figure. The lengths of the arm are also given as L1=1.5 m and L2=1.2 m. It is desired to determine the stress state of point A on the a-a section taken from the arm. The radius r of the section is r=0.012 m and the shear modulus of the arm material is G=75 Gpa. According to this; Question 2-A) Find the shear stress at point A due to the shear force. (Write your result in MPa.) Question 2-B) Find the shear stress due to the torsional moment at point A. (Write your result in MPa.) Question 2-C) Find the normal stress caused by the normal force at point A (Write your result in MPa.) Question 2-D) Find the normal stress caused by the bending moment at point A. (Write your result in MPa.)
Question 2) A force of magnitude F=28 kN, which makes an angle of θ=35 ° with the horizontal in the xz plane from point B, and a moment of magnitude M=18 kN.m from point C in the z direction acts on the arm in the figure. The lengths of the arm are also given as L1=1.5 m and L2=1.2 m. It is desired to determine the stress state of point A on the a-a section taken from the arm. The radius r of the section is r=0.012 m and the shear modulus of the arm material is G=75 Gpa. According to this; Question 2-C) Find the normal stress caused by the normal force at point A (Write your result in MPa.) Question 2-D) Find the normal stress caused by the bending moment at point A. (Write your result in MPa.)
Two loads P act as shown, one parallel to x and another parallel to z axes; each load P equals 1850 N. The crankshaft dimensions are b1 = 85 mm, b2 = 130 mm, and b3 = 60 mm. The diameter of the upper shaft is d = 28 mm. Determine the normal stress at point B, which is located on the surface of the upper shaft at the y axis. Lütfen birini seçin: a. 121.465 MPa b. 287,937 MPa O c. None O d. 149.606 MPa e. 324.676 MPa
The uniform 300-1b bar AB carries a 500-lb vertical force at A. The bar is supported by a pin at B and the 0.5-in. diameter cable CD. Find the stress in the cable. DRAW THE FREE BODY DIAGRAM.
The vertical load P acting on the wheel of a traveling crane is 13,000 lb. What is the average shear stress in the 1.25 in. diameter axle?
1) Determine the normal force at point E Express your answer to three significant figures and include the appropriate units. 2) Determine the shear force at point E. Express your answer to three significant figures and include the appropriate units. 3) Determine the moment at point E. Express your answer to three significant figures and include the appropriate units.
5/5 find the normal stress at left of point C A 100 C 40 kN 50 kN 40 mm 70 10 kN 20 mm 30 mm 100 mm 300 mm 300 mm 200mm B.
8&N 25 kN-m 5 kN Fig (1)

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