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

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

See similar textbooks

Related questions

Q: (a) Figure Q4 shows a composite body used in a certain application. Determine the centroid (x, y) of…

A: A composite crossection is given as follows

Q: 6. A three-block composite structure is loaded through rigid end plates, as s in the figure. What…

A: To find position of x such that end plates remain horizontal

Q: Problem #1: Determine the moment of inertia of the composite area about the y-axis and the the…

Q: onsano Acomposite assembly consisting of a steel [G- 80 GPa] core (2) connected by rigid plates at…

Q: 05/ B/Composite bar as shown in Fig.(4) carries the axial loads at the positions indicated and to…

A: Solution

Q: For the composite bar indicated, determine the permissible bending moment when the bar is bent about…

Q: Ac fab shc the

A: Deformation of column =0.72mm

Q: For the the composite cross-section shown in the figure, compute the following cross-seciton…

A: The composite cross-section shown in the figure. We need to compute the cross-seciton…

Q: 7. A solid aluminum cylinder is placed within an ASTM A501 steel tube as shown. Compute the stresses…

A: Given Data: The diameter of the solid aluminum cylinder is d1=3 in. The diameter of the steel tube…

Q: Problem 2. A W12×58 acts compositely with a 5-inch-thick concrete slab. The effective slab width is…

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: A composite bar BCD has a uniform external radius R, = 9cm. Segment BC is solid steel, while segment…

Q: For the composite figure shown, determine the centroidal moment of inertia about the x and y axes.

A: Th centroid of the body is the point where mass of the body is distributed evenly.The formula for…

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

Q: A composite bar BCD has a uniform external radius R. = 9cm. Segment BC is solid steel, while segment…

Q: A composite rod has 3 segments shown in Fig Q1. The diameters for each segment are given as; AB…

Q: 2.) GiVEN: The following cross secton Repersauts a composité cy lindere! FIND: a) the composite…

A: Centroid fomulay=Astyst+AmgymgAst+Amg Center of gravity isyCG=MStyst+MmgymgMst+Mmg

Q: a) Explain the performance metrics as an analytical methods for materials selection used in…

A: Given Diagram with stiffness and angle of twist equations To answer a) Explain the performance…

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

A: When rods are placed parallel as shown in the question, the torque applied to the assembly is shared…

Q: A composite beam is made of two brass [E = 105 GPa] plates bonded to an aluminum [E = 63 GPa] bar,…

A: Given data Eb = 105 GPA EAl = 63 GPA M= 1525 Nm = 1525 × 103 N-mm

Q: A compasite assembly consisting of a steel (G - 60 GPa) core (2) connected by rigid plates at the…

Q: SITUATION 1. A composite bar is made by attaching a copper rod of length 900 mm and diameter 30 mm…

Q: are Lec= 2 m and Lco= 1 m. The material moduli are Esteel = 200 GPa and Ecopper= 100 GPa. The bar is…

Q: Determine the centroidal moments of inertia of the symmetrical beam cross section shown- Determine…

A: GIVEN FIGURE:-

Q: A composite bar consists of aluminum and steel is held by rigid supports as shown. At 57°C, an axial…

Q: The composite shaft shown consists of a solid brass segment (1) and a solid aluminum segment (2)…

Q: A composite bar BCD has a uniform external radius R. = 9cm. Segment BC is solid steel, while segment…

Q: 1 0.25 m, width = 12 mm. The The following figure depicts an aluminum I beam of height h b= 0.2 m,…

A: Given: Dimensions of a composite T-beam are given. Axial load, P=500kN Modulus of elasticity for…

Q: A composite bar shown below made of steel and copper. The coefficients of expansion of steel and…

A: Given:- αs=α, αcu=1.25αEs=E, Ecu=0.5E

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 composite section is formed from a L 40x40x6, two L 80x40x6 and a 150mmx8mm plate as shown [consider the y-axis to be at the edge of the longer leg of the upper left L80x40x6]. Compute its moments of inertia about the centroidal x-axis and about the centroidal y-axis. (Answer for this question onwards.) Tabulate your solution for this. for L 40x40x6, area = 4.48 sq.cm, x = 1.2 cm, y = 1.2 cm, thickness = 6mm, Ix= 6.33 cm4, ly = 6.33 cm4; for L 80x40x6, area = 6.89 sq.cm, x=0.88 cm, y = 2.85 cm, thickness= 6mm, Ix 44.9 cm4, ly = 7.6 cm4;
Bar A-B-C is made from a fully bonded composite of two materials as shown in the cross section below. Find the Z displacement at point C. A C 1.10 m 20 kN B 1.25 m 50 kN с Y I cross section c-c Uz = 5 mm, material 1 5 mm, material 2 5 mm, material 1 25 mm Material 1 E = 240 (GPa) Material 2 E = 180 (GPa) mm (at C)
Q1 A cantilever composite beam is formed by bonding together brass bar (EB = 100 GPa) and aluminium (EA = 70 GPa) with cross section and loading at free end as shown in Figure Q1. Parameter x, y, and z are given by: X=0 Y=0 Z=2 (a) Determine the centroid and the moment of inertia of the composite section. (b) Calculate the maximum tensile and compressive stresses in the brass and aluminium. brass 5x mm (10 mm 20mm |4y mm 0.5(4y) mm M=2.z kN.m 4y mm aluminium Figure Q1 |
The composite bar is firmly attached to unyielding supports. The bar is stress-free at 50°F. Compute the stress in each material after the 80-kip force is applied and the temperature is increased to 100°F. Use a = 6.5 x106/°F for steel and a = 12.8 x106/°F for aluminum. Aluminum A = 2 in.² E = 10 x 106 psi 15 in. Steel A = 3 in.2 E = 29 × 106 psi 80 kips 10 in.
The composite bar shown is firmly attached to unyielding supports. An axial load P = 207 kN is applied at 26 ° C. Find the stress in each material at 63 °C. Assume a = 11.7 µm/(m-°C) for steel and 23 um/(m-C) for aluminum. Given: Ea = 75 GPa, Aa = 991 mm², La = 204 mm, Es = 213 GPa, As = 1,213 mm2, Ls = 318 mm. Answer must be in MPa. Aluminum Steel La Ls
A composite area is shown in the figure. Determine the radius of gyration about the x axis.
A composite bar BCD has a uniform extemal radius R, = (x+2) cm. Segment BC is solid steel, while segment CD is composed of a copper core of radius R;= 1cm bonded inside a steel sleeve. The lengths of the two segments are Lgc = 2 m and LCD= 1 m. The material moduli are Esel = 200 GPa and Ecoper = 100 GPa. The bar is fixed at B and tensile loads are applied at section D (FD = 1000 kN) and at section C (Fc = 400 kN). Compute the following: 1. Axial stress of steel in segment BC in MPa. 2. Axial stress of steel in segment CD in MPa. 3. Axial stress of copper in segment CD in MPa. 4. Total elongation of the assembly in mm. 2m в 1m 400 KN 1000 KN
A steel bar of 22 mm diameter and 8 cm gage length was axially loaded in tension and the following load deformation diagram was obtained. Determine: a) The yield strength by 0.2% off-set method. b) Modulus of elasticity by initial tangent method. c) Modulus of elasticity by tangent method at 2/3 of the yield strength. d) Modulus of elasticity by secant method at 70% of ultimate strength. e) Strain in fracture.
The composite A-36 steel bar shown is made from two segments, AB and BD, having cross-sectional areas of AB = 641 mm2 and BD = 1202 mm2 . Determine the vertical displacement (in mm) of end A. Modulus of Elasticity = 210 GPa. X = 1016 mm, Y = 790 mm, Z = 526 mm. Input the magnitude only. The answer is 0.58185. Show solution pls. Thank you.