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Spring Examinations 2009/2010: Mechanical and Biomedical Engineering, Exams of Materials science

Information about the spring examinations for the 3rd year modules in mechanical and biomedical engineering. It includes exam codes, module codes, paper details, instructions, requirements, and material properties for metallic alloys. Students are required to answer questions related to engineering stress-strain curves, crystallographic unit cells, burgers vectors, stress-strain curves for single crystals, and phase equilibrium diagrams.

Typology: Exams

2012/2013

Uploaded on 03/26/2013

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Spring Examinations 2009/ 2010
Exam Code(s)
3
BM,
3
BG
Exam(s)
3
rd
Mechanical
3
rd
Biomedical Engineering
Module Code(s)
ME326
Module(s)
Metals and Metal Processing
Paper No.
1
Repeat Paper
No
External Examiner(s)
Prof. Noel O’D
owd
Internal Examiner(s)
Prof. Sean Leen
Dr. Mark Bruzzi
Instructions:
Answer 3 questions
Duration
2 hours
No. of Pages
4
including cover sheet
Department(s)
Mechanical & Biomedical Engineering
Course Co
-
Dr. Mark Bruzzi
Requirements
:
Graph Paper
Yes
pf3
pf4

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Spring Examinations 2009/ 2010

Exam Code(s) 3 BM, 3 BG Exam(s) 3 rd^ Mechanical Engineering 3 rd Biomedical Engineering Module Code(s) (^) ME Module(s) Metals and Metal Processing Paper No. 1 Repeat Paper No External Examiner(s) Prof. Noel O’Dowd Internal Examiner(s) Prof. Sean Leen Dr. Mark Bruzzi Instructions: Answer 3 questions

Duration 2 hours

No. of Pages 4 including cover sheet Department(s) Mechanical & Biomedical Engineering Course Co-ordinator(s) Dr. Mark Bruzzi Requirements: Graph Paper Yes

1.(a) Table 1 gives the material properties of four metallic alloys. Using graph paper, sketch the engineering tensile stress-strain curves for each alloy. Clearly indicate how you used the data provided to construct the curves and label for one of the materials all the main features including: (i) Elastic and plastic regions (ii) Proof Stress (iii) Ductility (iv) Unloading curve and residual plasticity after a loading strain of 5% ( 8 ) Material Young’s Modulus (GPa) Yield Strength (MPa) Tensile Strength (MPa) Strain at Max. Stress % Fracture Strain Poisson’s Ratio 2024 Aluminium 70 345 485 0.13 18 0. Ti-6Al-4V 105 830 900 0.1 14 0. 304 Stainless Steel 205 515 860 0.085 10 0. Table 1: Tensile Mechanical Properties (b) A 10cm long, 10mm diameter cylindrical specimen of the 304 stainless steel, for which the stress-strain properties are given in Table 1, is pulled in tension with a force of 10kN. Compute the elongation and reduction in diameter of the specimen at its maximum load. ( 6 ) (c) If the specimen under consideration in part (b) is subjected to a torque, T, of 100 Nm, calculate the resulting angular deformation, , using: l

G

J

T 

J r

where l is the length of the bar, G is the shear modulus of the material and J is the polar moment of inertia given in terms of the radius of the bar r. (6)

4 .(a) Draw and clearly label a time-temperature transformation diagram for a eutectoid steel and draw continuous cooling curves for the transformation of austenite to: o Pearlite o Martensite o 50% Bainite + 50% Martensite Comment on the microstructure and associated mechanical behaviour of each. (6) (b) Outline and discuss the motivation for and the effects of adding alloying elements to carbon-iron alloys. (6) (c) In the carburising process for steel, a methane environment is used to set the surface carbon content to 1.2 wt %. If the initial carbon content in the steel is 0.25 wt %, calculate how long it will take at 950ºC for the carbon content to reach 0.8 wt % at a distance of 0.5mm from the surface. Assume that the diffusivity of carbon in steel at 950ºC is 1.6 x 10-^11 m^2 /s. (8) Table of Error Function Values where: x erf(x) x erf(x) x erf(x) 0.00 0.0000000 0.60 0.6038561 1.40 0.

  1. 05 0.0563720 0.65 0.6420293 1.50 0. 0.10 0.1124629 0.70 0.6778012 1.60 0. 0.15 0.1679960 0.75 0.7111556 1.70 0. 0.20 0.2227026 0.80 0.7421010 1.80 0. 0.25 0.2763264 0.85 0.7706681 1.90 0. 0.30 0.3286268 0.90 0.7969082 2.00 0. 0.35 0.3793821 0.95 0.8208908 2.20 0. 0.40 0.4283924 1.00 0.8427008 2.40^ 0. 0.45 0.4754817 1.10 0.8802051 2.60^ 0. 0.50 0.5204999 1.20 0.9103140 2.80^ 0. 0.55 0.5633234 1.30 0.9340079 3.0 0.