You are required to complete the Computational Methods coursework (CFD & FEA) using ANSYS and produce a professional technical report. All work must be carried out individually.
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## 1. Student Information
Student ID: 202421340
From this ID:
– A = 10 (since last digit = 0 use 10)
– B = 4
– E = 40 GPa
– P = 10 GPa (since last digit = 0 use 10)
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## 2. CFD Assignment
### Task 1: Flow Through a Bifurcated Tube
You are required to analyse water flow through a Y-shaped tube using CFD.
#### Geometry:
– Inlet diameter = 2A = 20 cm
– Outlet diameters = A = 10 cm each
– Element size = 0.00BA = 0.00410 m
#### Requirements:
1. Build the geometry in ANSYS.
2. Generate a high-quality mesh (include inflation layers near walls).
3. Apply boundary conditions:
– Velocity inlet
– Pressure outlets (0 Pa gauge)
4. Perform two simulations:
– Laminar flow
– Turbulent flow (Re > 4000)
#### Analysis:
– Calculate Reynolds number.
– Compare CFD results with theoretical values:
– Continuity equation
– DarcyWeisbach equation
– Use turbulence models:
– k- model
– k- SST model (for comparison)
– Clearly state turbulence model assumptions.
#### Outputs:
– Velocity contours
– Pressure contours
– Velocity profile (laminar vs theoretical parabola)
– Quantitative comparison (percentage error)
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### Task 2: Laminar Flow in a Nozzle
#### Given:
– Inlet height = 0.2 m
– Area reduction = 20%
#### Requirements:
1. Model the sinusoidal nozzle in ANSYS.
2. Apply laminar flow conditions.
3. Perform mesh independence study:
– Coarse, medium, fine meshes
4. Validate results using theory:
– Parabolic velocity profile
– Entrance length
– Pressure drop
#### Outputs:
– Velocity distribution
– Pressure distribution
– Mesh comparison table
– Convergence justification (< 2% variation)
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## 3. FEA Assignment
### Task 1: Tunnel Under External Pressure
#### Material Properties:
– Youngs Modulus = 40 GPa
– Poissons Ratio = 0.15
#### Loading:
– External pressure = 10 GPa
(Note: This value is unrealistically high and is used only for academic purposes based on Student ID.)
#### Boundary Conditions:
– Fixed support at the bottom
#### Requirements:
1. Model the tunnel geometry in ANSYS.
2. Apply pressure on top and side surfaces.
3. Perform structural analysis (plane strain).
#### Outputs:
– Maximum deformation
– Maximum von Mises stress
– Stress distribution plots
– Explanation of stress concentration locations
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### Task 2: Truss Bridge Analysis
#### Material:
– Youngs Modulus = 40 GPa
– Poissons Ratio = 0.29
#### Cross Section:
– A B = 10 mm 4 mm = 40 mm
#### Loading:
– Three point loads = 30 kN each
#### Boundary Conditions:
– Left: pinned support
– Right: roller support
#### Requirements:
1. Model the truss using LINK180 elements.
2. Apply loads and supports.
3. Perform structural analysis.
4. Validate results analytically (method of joints).
#### Outputs:
– Joint deflections
– Deformation plot
– Stress distribution
– Percentage error vs analytical results
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## 4. Simulation Settings (Important)
– Solver: Pressure-based solver (Fluent)
– Discretization: Second-order upwind
– Pressure-velocity coupling: SIMPLE
– Convergence criteria:
– Residuals < 110 (laminar)
– Residuals < 110 (turbulent)
– Mass imbalance < 0.1%
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## 5. Mesh Requirements
– Use multiple mesh sizes for validation
– Ensure:
– Skewness < 0.85
– Orthogonal quality > 0.15
– Include mesh images in report
– Demonstrate mesh independence
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## 6. Report Requirements
Prepare a professional report (maximum 8 pages) including:
### Sections:
1. Abstract
2. Introduction
3. Theory and Methodology
4. Results and Discussion
5. Conclusion
6. References
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### Important Notes:
– Include ANSYS figures (contours, mesh, deformation)
– Clearly label all figures and tables
– Compare CFD/FEA results with theory
– Include percentage error
– Discuss limitations (e.g., steady-state assumption, linear elasticity)
– Use clear academic English
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## 7. Submission Details
– Format: WORD
– Maximum length: 8 pages
– Submission via Moodle
– Deadline: As specified by the module
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Ensure all results are accurate, validated, and clearly explained. The work should demonstrate strong understanding of CFD and FEA principles and correct use of ANSYS tools.
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