The A-36 steel pipe in (Figure 1) has a 6061-T6 aluminum core. It is subjected to a tensile force of 200 kN. The pipe has an outer diameter of 81 mm and an inner diameter of 71 mm. For A-36 steel, Est = 200 GPa, and for 6061-T6 aluminum, Eal = 68.9 GPa. Figure < 1 of 1 > Determine the average normal stress in the aluminum due to this loading. Express your answer to three significant figures and include appropriate units. σal = Submit Part B μА Ost. = Value Request Answer 6 μA Determine the average normal stress in the steel due to this loading. Express your answer to three significant figures and include appropriate units. Value Units Ć ? Units ?

The A-36 steel pipe in (Figure 1) has a 6061-T6 aluminum core. It is subjected to a tensile force of 200 kN. The pipe has an outer diameter of 81 mm and an inner diameter of 71 mm. For A-36 steel, Est = 200 GPa, and for 6061-T6 aluminum, Eal = 68.9 GPa. Figure < 1 of 1 > Determine the average normal stress in the aluminum due to this loading. Express your answer to three significant figures and include appropriate units. σal = Submit Part B μА Ost. = Value Request Answer 6 μA Determine the average normal stress in the steel due to this loading. Express your answer to three significant figures and include appropriate units. Value Units Ć ? Units ?

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

PLEASE WRITE YOUR COMPLETE SOLUTION AND BOX THE FINAL ANSWER. THANK YOU. Determine the normal stress and change in length of the aluminum rod if the temperature was raised by 126°C. The 0.5-mm gap exists at 27°C.
(3) The cantilever bar as shown on next page is made of a brittle material. At D, Fx-300 lb. F-250 lb, and F-100 lb. Determine the precise location of critical stress element at the cross section at A. Determine the magnitude for each of the stress components considering the stress concentration at A. Find the principal stresses and the maximum shear stress at this location. 2 in 1-in dia. -in R. 12 in
7 Principal stresses of a point in a critical section of a machine component are: ₁= 80 MPa 0₂= 5 MPa 03 = -60 MPa Tensile yield strength is, oy = 200 MPa According to the maximum shear stress theory. Determine factor of fafety ?
A cylindrical tank steel pressure vessel 200mm in radius and 4.0m in length, is subjected to an internal pressure of 3.0 MPa. Determine the thickness of tank (nearest mm) if the following stresses are not to be exceeded: tangential stress of 45 MPa and longitudinal stress of 30 MPa. and also show the free body diagram
Determine the pricipal stresses and the directions of the principal stresses at points A Refer to Figure P18-50
The tank of the air compressor is subjected to an internal pressure of 0.43 MPa as shown in (Figure 1). The internal diameter of the tank is 550 mm, and the wall thickness is 6 mm. Figure ⁹-1 Y Y Part A Determine the hoop stress acting at point A. Express your answer to three significant figures and include the appropriate units. 0 = Submit Part B 02 = Submit O Provide Feedback HA Value Request Answer Determine the longitudinal stress acting at point A. Express your answer to three significant figures and include the appropriate units. Value HÅ 1 h Units Request Answer Units ? F ?
100 kip 10 kip ft The 4-in. diameter shaft shown above is made from a ductile brass alloy. Which of the following are closest to the principal stresses in the shaft? 01 = 31.8 ksi 02 = 76.4 ksi = 94.0 ksi 02 = -62.1 ksi O0g - 14.3 ksi 02 = -6.37 ksi Oo= 7.96 ksi 02 = 9.55 ksi
The copper pipe [G = 7,000 ksi] has an outside diameter of 3.000 in. and a wall thickness of 0.125 in. The pipe is subjected to a uniformly distributed torque of t= 70 Ib-ft/ft along its entire length. Using a = 2.0 ft, b = 4.0 ft, and c = 8.5 ft, determine (a) the maximum shear stress in the pipe. (b) the rotation angle oc at the free end of the shaft. B Answers: (a) Tmax = i psi (b) Фс- і rad
How to find circumferencial stress in the cylindrical vessel. Give the equations.
The state of stress at a point in a component is ox = -14 ksi, oy = -20 ksi, Txy-4 ksi. Sketch the state of stress at the point in x-y and the calculate the principal stresses and the magnitude of the maximum shear stress. OA = ksi OB ksi Magnitide of tmax ksi %D
Determine the average normal stress at points A, B, and C. The diameter of each segment is indicated in the figure.
69. A disc of 600 mm diameter and uniform thickness is rotating at 3000 rpm. Calculate the maximum stress developed in the disc. If a hole of 100 mm dianmeter is drilled at the centre of the disc, then determine maximum radial and hoop stresses developed. Take vs 0-28 and p = 7800 kg/m.