a. Calculate the largest tensile and compressive stresses that occur in section a-a shown in the figure, b. Show the distribution of normal stresses by drawing along the height of the section, c. Tensile safe tensioning of the clamp material of 50 MPa and compression-safe stress o= 80 MPa, the biggest compression that can be applied without damaging the a-a section

a. Calculate the largest tensile and compressive stresses that occur in section a-a shown in the figure, b. Show the distribution of normal stresses by drawing along the height of the section, c. Tensile safe tensioning of the clamp material of 50 MPa and compression-safe stress o= 80 MPa, the biggest compression that can be applied without damaging the a-a section

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

Related questions

Q: Axial loads are applied with rigid bearing plates to the solid cylindrical rods shown. The normal…

Q: A beam with the cross section geometry and dimensions as shown in the figure and parameter table is…

A: “Since you have posted a question with multiple sub parts, we will provide the solution only to the…

Q: Ql; A bar ABCD shown in Figure (1) below consists of three sections: AB is of 42 mm diameter and 80…

Q: The figure shows a roof truss and the detail of the connection at joint B. Member BC and BE are…

Q: Calculate the bearing stress and shear stress between the pin and each bracket of a clevis joint.…

Q: Find the normal stress and shear stress in the c-plane for the stressed member shown in the figure.…

A: Given figure To determine the normal stress and shear stress in the c-plane for the stressed…

Q: ess of bar: 6 m mm mm adius, r= 4 mm

Q: 4. Solve problem 8.10 in our textbook (find the safety factor for failure at the fillet). Note that…

Q: A cylindrical bar shown in the figure below has axial loads applied as illustrated Calculate the…

Q: The cantilevered bar in the figure is made from a ductile material and is statically loaded with Fx…

A: Given data:The values of forces are given as: Fx = 300 lbf, Fy = 250 lbf, and Fz = –100 lbf.Here,…

Q: Required information The cantilevered bar in the figure is made from a ductile material and is…

A: The cantilever beam static load given as, Fy= 380 lbf The diameter of the beam is given as, D= 3 in…

Q: A square pedestal has glued parts at joints t, r, e, and s. Plane t-r-e-s is at anole of 30° from…

A: Given: The allowable compressive stress = 5.2 Mpa The inclination of plane = 30 degree The shear…

Q: A single-piece bicycle crank is shown below under the following load: the rider pedals forward with…

Q: The figure shows a roof truss and the detail of connection at joint I. The allowable stresses are 70…

Q: Why As is like 2(pi/4)d^2 This question asks for the average tension only in section a-a, is that…

A: As we can see that section a-a will be in shear and not in tension.

Q: For the clamp C shown in the figure, determine the maximum clamping force P if the normal tension…

A: Introduction: Clamping force is the amount of force imparted to a workpiece by closing and locking a…

Q: For P=8.5kN, determine the allowable stress if the thickness t is 20 mm. Section Properties At the…

Q: 4. The figure shows a riveted lap joint with cover plates connecting two steel plates. Each rivet…

Q: Complete answer

A: Given Data: Diameter of OB and AB (D) = 100 mm = 0.1 m Radius of disc (r) = 0.5 m Allowable normal…

Q: 6.* Figure 6 shows two plates of thickness t = 6 mm and width (into the paper) 50 mm tha are joined…

A: please refer handwritten solution

Q: 03: For the cyclic stress shown in the figure (aside) calculate: 1. The mean stress 2. The range of…

Q: Problem 1-3 The Cartesian components of stresses at a point are given as belou : O = 7, 0y = 6, oz =…

A: The cartesian components of stresses at a position specified in the inquiry are known to us :…

Q: Question 2) arm of Figure B from point x z plane, a horizontal angle of θ = 38 ° angled F = 29…

Q: ember BED is supported using steel rods AB, CD, and EF as shown below. E-20 If a force P is applied…

A: GivenL1=425mmL2=320mmP=8kNAAB=310mm2ACD=310mm2AEF=420mm2E=200GPa

Q: Flat steel A is welded to the wall as shown in the figure. The profile of the flat steel is…

A: Based on the image you sent, I can't access the specific data points to solve for the median grain…

Q: A compression load of P = 50 kips is applied to a 2 in. by 2 in. square post, as shown. Determine…

Q: Ql:A bronze bar is fastened between a steel bar and an aluminum bar as shown in Fig. Axial loads are…

A: Answer: The largest allowable value of P is 7.12225 kN.

Q: a) Construct a rigid body force diagram of the arm with appropriate labels for all forces and the…

Q: A hook as shown in figure 2 is a symmetrical trapezium of 50 mm deep, the inner width being 60 mm…

Q: Check whether the A-A section is safe in the hand vice in the figure. 2mm diameter 8mm size copper…

A: Given: The allowable stress for material, Sall = 140 MPa The moment of inertia about x-axis, Ix =…

Q: The stress concentration occurs whenever there is an abrupt change in the cross-section of a…

A: Stress concentration Factor (k) : it is defined as the localisation of higher stresses due to…

Q: 10 rivets are fastened on a lap joint of 1.25 inch in diameter the thickness of the lap join were…

A: Given: Number of rivets→n=10 Diameter of the each rivet→d=1.25 inch Hence area for shear…

Q: –L2 H K F1 L1 F2

Q: Oy = 90MPA %3D Try 60MPA %3D Ox=20MPA

A: Given Data Normal stresses σx= 20MPa σy=90MPa Shear stress fxy=60MPa Main stresses are the…

Q: See the figure below. AD is a member with varying diameters. There are three axial loads applied at…

A: Given data: The magnitude of the force acting at the point B is; F1=10 lbs. The magnitude of the…

Q: A lap joint, consisting of 250 mm × 75 mm wooden plates, is fastened with two(2) rows of 20 mm…

A: Width = 250 mm Thickness = 75 mm Diameter of rivet = 20 mm No. of rivets = 6 Shear stress = 70 MPa…

Q: For the assembly shown in Figure 2, the cross section of the pipe at section B has outer diameter of…

A: Consider the diagram shown below for the given hollow shaft. The twist moment at the vertical…

Concept explainers

Pressure Vessels

The term pressure vessel refers to a closed container that contains gas or liquid at a different pressure than environment pressure. The pressure vessels have a wide scale of applications in our day-to-day lives and other industrial places. Some common examples of pressure vessels are gas cylinders, autoclaves, compressor vessels, etc.

Question

100%

a. Calculate the largest tensile and compressive stresses that occur in section a-a shown in the
figure,
b. Show the distribution of normal stresses by drawing along the height of the section,
c. Tensile safe tensioning of the clamp material of 50 MPa and compression-safe stress
o= 80 MPa, the biggest compression that can be applied without damaging the a-a section

Expert Solution

This question has been solved!

Explore an expertly crafted, step-by-step solution for a thorough understanding of key concepts.

This is a popular solution!

SEE SOLUTION Check out a sample Q&A here

Step 1

Step 2

Step 3

Step 4

Trending now

This is a popular solution!

Step by step

Solved in 4 steps with 6 images

SEE SOLUTION Check out a sample Q&A here

Knowledge Booster

Learn more about

Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, mechanical-engineering and related others by exploring similar questions and additional content below.

Similar questions

Figure shows a beam made from bronze subjected to a 3.5kN.m bending couple and its respective tensile properties. i) With aid of illustration, draw the deformation of the bean and locate the position where the beam experience maximum tensile stress (αmax)t and maximum compressive stress (αmax)c. Accordingly. Determine the magnitude of these two stresses. ii) Sketch the two-dimensional stress distribution acting on point A and point B over the cross-sectional area of the beam as observed from side view. Estimate the magnitude of the stresses at those two points.
Read the question carefully and give me answer according to the question
A wood structure is assembled to support the force applied. All pieces of wood have a width of 5 in. The normal failure stress of the wood is o fail = 6000 psi. The shear failure stress of the wood is T fail = 2500 psi. The factor of safety against failure is 5. Hint: 1. Analyze the whole structure first to find the normal forces in members AB and AC b B 0₁ ᎾᎥ z F A F 01 0₁ C Values for the figure are given in the following table. Note the figure may not be to scate.
Calculate the internal force (positive if tensile, negative if compresive) in rod (2). Use a FBD cutting through the rod in the section that includes the free end A.Answer: F2 = ? kips
The figure shows a riveted lap joint with cover plates connecting two steel plates. Each rivet has diameter of 12 mm and the thickness of each steel plate is 15 mm. (a) Compute the shear stress (MPa) in each rivet due to a force of 10.2 kN applied to the plates. (b) If the bearing stress in the steel plates is limited to 40 MPa, what is the allowable load P (kN)? (c) If the width of the steel plates is 100 mm what is the allowable load P (kN) for a limited normal stress of 20 MPa?
2. The bar ABCD in the given figure below consist of three (3) cylindrical steel segments, each with a different cross-sectional area. Axial load are applied as shown. Calculate the normal stress in each segment. 15000 lbs 20000 lbs D. 10000 Ibs A A=1.6 sq. in |B A=1.4 sq. in A=1.2 sq. in 2ft- 1.5 ft 1.2ft
Find p1 and p2
5 Figure 5 shows a thick cylinder of 50 mm internal radius and 115 mm outer radius is subjected to an internal pressure of 60 MN/m² and an extemal pressure of 30 MN/m?. Determine the hoop and radial stresses at the inside and outside of the cylinder together with the longitudinal stress if the cylinder is assumed to have closed ends using analytical and graphical approaches.
The magnitude of force (F) if Al = 0.06 m: F = kx F = (500)(0.06) F = 30 N Homework A hollow cylinder 2 m long has an outside diameter of 50mm and inside diameter of 30mm. If the cylinder is carrying a load of 25 KN. FInd the stress in cylinder, also find deformation of the cylinder E=100 Gpa. (Ans: Stress=20.0 N/mm2, Deformation= 0.4 mm) A load of 5KN is to be raised with the help of a steel wire. Find the minimum diameter of wire if stress is not to exceed 100 MPa. For more solved problems: (Ans: d=7.98mm)
Define the main difference between thick and thin cylinders and give an example for each type of cylinder Derive the expression of longitudinal stress, o, for a closed thick cylinder which has inner radius, R₁ and outer radius, R₂ and subjected to internal pressure only. Figure Q3 shows a cross section of composite cylinder that is made by shrinking a tube of 330 mm internal diameter and 50 mm thick over another tube of 330 mm external diameter and 50 mm thick. The radial pressure at the common surface, after shrinking is 180 MPa. Suppose the compound cylinder is subjected to an internal fluid pressure of 1200 MPa, determine; i) the hoop stresses at inner radius and outer radius of inner cylinder, ii) the hoop stresses at inner radius and outer radius of outer cylinder. Ro P Figure Q3 R₁
The bar in the figure with a diameter of 25 mm and a length of 1000 mm is made of Ti6Al4V alloy. A to this bar A force of 1000 N is applied with an arm of 800 mm length from the point. this force (a) the highest stress in the bar, (b) the type of stress, (c) the location of this stress (d) calculate how many degrees the rod rotates under the effect of this force. (Module of Elasticity of Ti6Al4V alloy 105 GPa and Poisson's ratio is 0.3).
Question 2) arm of Figure B from point x z plane, a horizontal angle of θ = 38 ° angled F = 29 kN force sized and C from the point z direction M = 17 kn.m acts a moment in size. The lengths of the arm are also given as L 1 = 1.5 m and L 2 = 1.1 m . It is desired to determine the stress state of point A on the aa section taken from the arm. The radius r of the section is r=0.015 m and the shear modulus of the arm material is also G = 78 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. (Your result MPa in the size of your font.)