A cast iron link has dimension of 40 x 200 x 500 mm as shown in the figure. Thecompressive load P = 400 kN is applied to the ends of the link along a longitudinal axis thatis located 150 mm above the bottom of the link (50 mm above the neutral axis). Determinethe normal stress developed at the bottom surface point A.50 mmNA-150 mm200 mmA500 mm40 mm

Calculate compressive stress and bending stress at point A

Answered: A cast iron link has dimension of 40 x…

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

Need Step wise solution
The principal strains at a point on the aluminum surface of a tank are P1 = 630(10-6) and P2 = 350(10-6). If this is a case of plane stress, determine the associated principal stresses at the point in the same plane. Eal = 10(103) ksi,nal = 0.33.
For the assembly shown in the figure helow, Determine the state of stress at point A on the cross section of the pipe at section a-a. 20 mm P= 250 a= 240 b= 140 d= 25 Soction a-a
Determine the nodal displacements and the element stresses. E = 105 GPa, v = 0.3, and t = 5 mm. You don't have to calculate everything manually, but can write a code to get some input from you and find the stiffness matrices for instance. 400 mm 3 5 400 mm 30 kN 2
The rectangular bar is connected to the support bracket with a 25-mm-diameter pin. The bar width is w = 65 mm and the bar thickness is 10 mm. Each side of the bracket has the same dimensions as the bar. The average shear stress in the pin cannot exceed 115 MPa, the bearing stress in the bar cannot exceed 120 MPa, and the bearing stress in the bracket cannot exceed 140 MPa. Determine the maximum value of Pmax that can be supported by the structure. Answer: Pmax i kN
A 30 mm square is drawn on the rim of a large steel pressure vessel. The biaxial stress situation in the square after the pressure is applied is as shown in the figure. Determine the change in length of the BC edge in (mm).
Part 1. A composite assembly of length, L-375 mm, consisting of a steel (G-77 GPa) core (2) connected by rigid plates at the ends of an aluminum [G-35 GPa) tube (1) is shown. The aluminum tube has outside diameter D₁ - 50 mm and inside diameter d₁-30 mm. = 100 MPa, and the The solid steel core has diameter d₂-25 mm. The allowable shear stress of aluminum tube (1) is (rallow) allowable shear stress of steel core (2) is (Tallow)2= 135 MPa. Determine (a) the allowable torque T that can be applied to the composite shaft. (b) the corresponding torques produced in tube (1) and core (2). (c) the angle of twist produced by the allowable torque T. T D₁ L Calculate the polar moment of inertia, J₁, of the aluminum tube. Answer: J₁ (106) mm².
Based on the figure below, a pin supports a bar at Z and a cable supports X to Y around W. Determine the stress in the cable in megapascal with a diameter of 0.68 inch and a weight of 1,550 pounds. a = = 1 ft b= 3 ft c = 10 ft X bft Y W aft cft Z
P to point A of the section given in the figure Plot the normal stress distribution in the section, given that a compressive force of = 20 kN is applied.
ANSWER ASAAAAP PLS
Find the stresses in each section and total change in length of the bar as shown in figure. The bar is subjected to an axial pull of 24 kN. Take the diameter of section 1 as 56 mm, length L1 as 44 mm, ,the dimensions of section 2 as 65 mm x 63 mm, L2 as 16 mm, section 3 is a square of size 30 mm, length L3 as 50 mm. Also take the Young’s modulus of sections as E1 = 2.1x105 N/mm2, E2 = 1.1x105 N/mm2, E3 = 0.75x105 N/mm2 (i) Stress in section 1 (unit in N/mm2) is = Answer for part 1 (ii) Stress in section 2 (unit in N/mm2) is = Answer for part 2 (iii) Stress in section 3 (unit in N/mm2) is = Answer for part 3 (iv) Total Change in length of the given bar (unit in mm) is =

Recommended textbooks for you

Elements Of Electromagnetics

Mechanical Engineering

ISBN:

9780190698614

Author:

Sadiku, Matthew N. O.

Publisher:

Oxford University Press

Mechanics of Materials (10th Edition)

Mechanical Engineering

ISBN:

9780134319650

Author:

Russell C. Hibbeler

Publisher:

PEARSON

Thermodynamics: An Engineering Approach

Mechanical Engineering

ISBN:

9781259822674

Author:

Yunus A. Cengel Dr., Michael A. Boles

Publisher:

McGraw-Hill Education

Elements Of Electromagnetics

Mechanical Engineering

ISBN:

9780190698614

Author:

Sadiku, Matthew N. O.

Publisher:

Oxford University Press

Mechanics of Materials (10th Edition)

Mechanical Engineering

ISBN:

9780134319650

Author:

Russell C. Hibbeler

Publisher:

PEARSON

Thermodynamics: An Engineering Approach

Mechanical Engineering

ISBN:

9781259822674

Author:

Yunus A. Cengel Dr., Michael A. Boles

Publisher:

McGraw-Hill Education

Control Systems Engineering

Mechanical Engineering

ISBN:

9781118170519

Author:

Norman S. Nise

Publisher:

WILEY

Mechanics of Materials (MindTap Course List)

Mechanical Engineering

ISBN:

9781337093347

Author:

Barry J. Goodno, James M. Gere

Publisher:

Cengage Learning

Engineering Mechanics: Statics

Mechanical Engineering

ISBN:

9781118807330

Author:

James L. Meriam, L. G. Kraige, J. N. Bolton

Publisher:

WILEY

SEE MORE TEXTBOOKS