A composite assembly consisting of a steel [G-80 GPa] core (2) connected by rigid plates at the ends of an aluminum [G = 28 GPa]tube (1) is shown. The cross-sectional dimensions of the assembly are shown in the second figure. Assume L= 280 mm, D1-58, d1= 37mm, d2= 20 mm. If a torque of T-800 N-m is applied to the composite assembly, determine(a) the maximum shear stress in the aluminum tube and in the steel core.(b) the rotation angle of end B relative to end A.(1)(2)BL.(1)diAnswers:MPa(a) Talum =MPaTsgeel =rad(b) P-PA =

maximum shear stress : The highest shear stress in a short area is the most concentrated shear…

A composite assembly consisting of a steel [G-80 GPa] core (2) connected by rigid plates at the ends of an aluminum [G - 28 GPa] tube (1) is shown. The cross-sectional dimensions of the assembly are shown in the second figure. Assume L-280 mm, D1-58, d-37 mm, d2- 20 mm. If a torque of T-800 N-m is applied to the composite assembly, determine (a) the maximum shear stress in the aluminum tube and in the steel core. (b) the rotation angle of end B relative to end A. (1) (2) T. (1) d2 D1

A composite assembly consisting of a steel [G-80 GPa] core (2) connected by rigid plates at the ends of an aluminum [G - 28 GPa] tube (1) is shown. The cross-sectional dimensions of the assembly are shown in the second figure. Assume L-280 mm, D1-58, d-37 mm, d2- 20 mm. If a torque of T-800 N-m is applied to the composite assembly, determine (a) the maximum shear stress in the aluminum tube and in the steel core. (b) the rotation angle of end B relative to end A. (1) (2) T. (1) d2 D1

Steel Design (Activate Learning with these NEW titles from Engineering!)

6th Edition

ISBN:9781337094740

Author:Segui, William T.

Publisher:Segui, William T.

Chapter1: Introduction

Section: Chapter Questions

Problem 1.5.6P: The data in Table 1.5.3 were obtained from a tensile test of a metal specimen with a rectangular...

See similar textbooks

Related questions

Q: See the image below. A hot-rolled l-beam section has yield strength 300 MPa, ultimate ength 320 MPa.…

Q: The composite plate is made from both steel (A) and brass (B) segments. Determine the mass and…

A: Consider the following diagram having the division of element A into two parts:

Q: The composite shaft shown in the figure consists of a bronze sleeve (1) securely bonded to an inner…

A: Given data, D1 = 35 mm d1 = 20 mm G1 = 41 GPa D2 = 20 mm G2 = 80 GPa L = 430 mm T = 990 N-m To find…

Q: For the built-up shape shown, determine: (a) the elastic section modulus and the yield moment (b)…

Q: The A-36 steel column is encased in high-strength concrete as shown. If an axial force of 60 kip is…

Q: (a) the maximum shear stresses in the bronze sleeve and the steel core. (b) the rotation angle of…

Q: The following data were obtained from the tensile test of Aluminum alloy. The initial diameter of…

A: Following is the graph deduced from the given information in the table: Part a. Proportional…

Q: Problem 2: A composite shaft is composed of a solid section AB and a tubular section BC, both of…

Q: The wood beam has a rectangular cross section in the proportion shown. The allowable bending stress…

Q: consists of a H.W.7: The composite shaft shown in Figure solid brass segment (1) and a solid…

Q: t AB, BC and CD is 35 mm, 40 mm and 30 mm, respectively. The elastic modulus fo um is 72.4 x 10'…

Q: The ABC steel rod is attached to rigid supports and is unstressed at a temperature of 20°C. The…

Q: The composite bar is firmly attached to unyielding supports. The bar is stress-free at 50°F. Compute…

Q: The composite shaft showWn in Figure consists of a solid brass segment (1) and a solid aluminum…

A: when shafts are connected in series, Due to application of torque rotation will be the same in both…

Question

A composite assembly consisting of a steel [G-80 GPa] core (2) connected by rigid plates at the ends of an aluminum [G = 28 GPa]
tube (1) is shown. The cross-sectional dimensions of the assembly are shown in the second figure. Assume L= 280 mm, D1-58, d1= 37
mm, d2= 20 mm. If a torque of T-800 N-m is applied to the composite assembly, determine
(a) the maximum shear stress in the aluminum tube and in the steel core.
(b) the rotation angle of end B relative to end A.
(1)
(2)
B
L.
(1)
di
Answers:
MPa
(a) Talum =
MPa
Tsgeel =
rad
(b) P-PA =

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

VIEW

Step 2

VIEW

Step 3

VIEW

Trending now

This is a popular solution!

Step by step

Solved in 3 steps with 1 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, civil-engineering and related others by exploring similar questions and additional content below.

Similar questions

A tensile test was performed on a metal specimen having a circular cross section with a diameter 0. 510 inch. For each increment of load applied, the strain was directly determined by means of a strain gage attached to the specimen. The results are, shown in Table: 1.5.1. a. Prepare a table of stress and strain. b. Plot these data to obtain a stress-strain curve. Do not connect the data points; draw a best-fit straight line through them. c. Determine the modulus of elasticity as the slope of the best-fit line.
The results of a tensile test are shown in Table 1.5.2. The test was performed on a metal specimen with a circular cross section. The diameter was 3 8 inch and the gage length (The length over which the elongation is measured) was 2 inches. a. Use the data in Table 1.5.2 to produce a table of stress and strain values. b. Plot the stress-strain data and draw a best-fit curve. c. Compute the, modulus of elasticity from the initial slope of the curve. d. Estimate the yield stress.
A tensile test was performed on a metal specimen having a circular cross section with a diameter of 1 2 inch. The gage length (the length over which the elongation is measured) is 2 inches. For a load 13.5 kips, the elongation was 4.6610 3 inches. If the load is assumed to be within the linear elastic rang: of the material, determine the modulus of elasticity.
Compare the engineering and true secant elastic moduli for the natural rubber in Example Problem 6.2 at an engineering strain of 6.0. Assume that the deformation is all elastic.
In Example Problem 12.1, a uniaxial composite material is made into a circular rod Vbith a 1.27-cm diameter from 70 volume percent continuous carbon fibers and 30 volume percent epoxy. The rod is subject to an axial force of 100,000 N. The composite matcrial in Example Problem 12.1 is to be replaced with a less expensive composite made of 70 volume percent continuous E-glass fibers and 30 volume percent epoxy. The elastic moduli are 5 GPa for the epoxy resin and 72.4 GPa fos the E-glass. (a) Compare the elastic modulus, composite strain, fiber and matrix stresses, and density of this composite with the carbon epoxy composite in Example Problem 12.1. Usc the density of UHM carbon, and assume the density of the epoxy is 1.2g/cm3 . (b) Can both the E-glass fiber and matrix withstand the applied force?
A tensile test was performed on a metal specimen with a diameter of 1 2 inch and a gage length (the length over which the elongation is measured) of 4 inches. The dam were plotted on a load-displacement graph. P vs. L. A best-fit line was drawn through the points, and the slope of the straight-line portion was calculated to be P/L =1392 kips/in. What is the modulus of elasticity?
Estimate the transverse tensile strength of the concrete in Problem 12.6.
The frame of a space shuttle type vehicle must have a high yield strength and high stillness, and the most important design factor is weight. Of all the materials presented in this chapter, what material might be the most suitable for the frame of a space shuttle? Assume that there will be both tensile and compressive stresses. For a space shuttle, cost is not a limiting factor. (a) You can eliminate entire classes of materials from consideration with a brief statement about their unsuitability. (b) What material has the highest specific yield strength? Give the yield strength, specific gravity, specific yield strength, elastic modulus, and specific elastic modulus for this material. (c) What material has the highest specific elastic modulus? Give the yield strength, specific gravity, specific yield strength, elastic modulus, and specific elastic modulus for this material. (d) Compare the materials with the highest specific yield strength and highest specific elastic modulus for suitability in the space shuttle frame. (C) Discuss the suitability of the top-rated material for this design from the viewpoint of the ability to produce a frame.
According to Figure 5-20, is ii possible to completely separate one of the four materials from the other three? Explain your answer.
In concrete work, Fuller and Thompson (1907) suggested that a dense packing of grains can be achieved if the percent finer (p) and grain size (D) are related by the following equation, where n is a constant varying in the range of 0.3-0.6. Dmax is the size of the largest grain within the soil. p=(DDmax)n100 This equation is sometimes used in roadwork for selecting the aggregates. a. For n = 0.5, show that the soil is well graded. b. If n = 0.5 and Dmax = 19.0 mm, find the percentages of gravel, sand, and fines within the soil. Use the Unified Soil Classification System.