Assignment Task Brief Mechanics of Materials (Group 30)
You are required to complete a full engineering analysis and design report based on the provided assignment brief. The work must be carried out individually and presented professionally, as it will be assessed through a 30-minute presentation and viva session.
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Overall Objective
Deliver a complete, well-structured engineering solution that demonstrates strong understanding of stress analysis, fatigue, and mechanical design principles. The work must include clear methodology, justified assumptions, accurate calculations, and critical discussion.
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Question 1 Shaft Analysis (60 Marks)
You are required to analyse a hollow steel shaft subjected to combined cyclic loading.
### Given (Group 30 Data)
– Hole diameter (a) = 6 mm
– Outer diameter (D) = 36 mm
– Material = AISI 1030 CD
– Torque = 120 Nm (completely reversed)
– Bending moment = 150 Nm (completely reversed)
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## Task 1(a): Factor of Safety Analysis
Perform a complete fatigue and static failure analysis using:
– Gerber fatigue criterion
– Langer static yield criterion
### Requirements:
– Determine stresses due to bending and torsion
– Include stress concentration effects (due to hole)
– Calculate alternating and mean stresses
– Determine factor of safety for:
– Fatigue failure
– Static failure
– Present S-N curve clearly
– Use spreadsheet or MATLAB where appropriate (with explanation)
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## Task 1(b): Literature Review
Provide a critical discussion on:
– The role of Factor of Safety in fatigue design
– How it influences fatigue life prediction
– Trade-offs between safety, weight, and cost
Support your discussion with academic references.
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## Task 1(c): Hollow Shaft Design Process
Conduct a literature-based discussion covering:
– Material selection criteria
– Geometric optimization (diameter, thickness, fillets)
– Methods to reduce stress concentration
– Failure modes (fatigue crack initiation & propagation)
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# Question 2 Aircraft Door Handle Design (40 Marks)
You are required to design a structural component (door handle) under load.
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## Task 2(a): Material Selection
Select a suitable aircraft-grade aluminum alloy.
### Requirements:
– Justify selection based on:
– Strength-to-weight ratio
– Fatigue resistance
– Corrosion resistance
– Support with material data and references
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## Task 2(b): Stress Analysis & Design
Design the component to safely withstand the applied force.
### Requirements:
– Calculate stresses at the critical location
– Determine:
– Principal stresses
– Maximum shear stress
– von Mises stress
– Identify critical planes
– Apply an appropriate failure criterion
– Ensure a reasonable Factor of Safety
– Provide clear diagrams and stress representation
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## Task 2(c): Experimental Validation
Explain how you would independently verify material properties:
– Describe testing methods (e.g., tensile, fatigue tests)
– Identify relevant engineering standards
– Explain specimen preparation and data extraction
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# Deliverables
## 1. Engineering Report
– Structured, clear, and detailed
– Includes all calculations, diagrams, and references
– Logical flow and justified decisions
## 2. Spreadsheet / Numerical Work
– All calculations clearly shown
– Proper use of formulas
– Well-organized and labeled
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# Presentation & Viva (IMPORTANT)
The assessment will be conducted as follows:
### First 15 minutes Presentation
You must:
– Clearly explain your methodology
– Present key results and findings
– Use visuals (graphs, diagrams, stress plots)
### Next 15 minutes Viva (Q&A)
You must be able to:
– Justify your assumptions
– Explain every step of your calculations
– Discuss design decisions confidently
– Demonstrate full understanding (not memorization)
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# Key Expectations
– All work must be original
– No plagiarism or collaboration
– Clear reasoning is more important than final answers
– Engineering judgement is essential
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# Final Note
– Stress Analysis
– Fatigue Behaviour
– Mechanical Design Principles
Ensure the work is professional, defensible, and presentation-read
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