MODULAR PROGRAMME- COURSEWORK ASSESSMENT SPECIFICATION
Module Details
Module Code
UFMFVL-15-M
|
Run
24/25
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Module Title
Mechanics of Composites
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1 Introduction
This coursework is a team-based activity. Pair in groups of 2 and address Tasks 1 and 2.
2 Task 1- Laminate Analysis 35%
A laminate is made of n laminae each from different materials is subjected to three membrane forces and three bending moments as shown in Figure 1.
Figure 1: A laminate subjected to membrane forces and bending moments
where
• Nx = normal force resultant in the x direction (N/m)
• Ny = normal force resultant in they direction (N/m)
• Nxy = shear force resultant (N/m)
• Mx = Bending moment resultant in the x direction (N. m/m)
• My = Bending moment resultant in they direction (N. m/m)
• Mxy = Torsional moment resultant (N. m/m)
This laminate is made of nplies ( n ≤ 11) each having a thickness of tk and an angle of θk with the x axis (global coordinate). The material properties of one ply in its principal directions are given in Table 1.
Table 1: Mechanical properties of composite ply
E11
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Longitudinal modulus of elasticity (Mpa)
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E22
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Transverse modulus of elasticity (Mpa)
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G12
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In-plane shear modulus (Mpa)
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Xt
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Tensile strength of ply in longitudinal direction (Mpa)
|
Xc
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Compressive strength of ply in longitudinal direction (Mpa)
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Yt
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Tensile strength of ply in transverse direction (Mpa)
|
Yc
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Compressive strength of ply in transverse direction (Mpa)
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S
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In-plane shear strength (Mpa)
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θ12
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Poisson's ratio in plane 1-2
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α1
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Longitudinal coefficient of thermal expansion (μE/℃)
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α2
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Transverse coefficient of thermal expansion (μE/℃)
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β1 *
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Longitudinal moisture swelling coefficient (μE/%)
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β2
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Transverse moisture swelling coefficient (μE/%)
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* Strain is measured in μE and ∆c (change in concentration of the swelling agent, i.e. moisture) is percentage (%)
2.1 Part A- 20%
The laminate is subjected to membrane forces, bending moment, change of temperature ΔT and a moisture concentration of Δc. Design an interactive spreadsheet to calculate the:
1. Factor of Safety (FoS) of each ply and the whole laminate based on maximum stress criterion.
2. FoS of each ply and the whole laminate based on maximum strain criterion
3. FoS of each ply and the whole laminate based on Tsai-Hill Criterion.
4. FoS of each ply and the whole laminate based on Tsai-Wu Criterion.
5. FoS of each ply and the whole laminate based on Hoffman criterion.
2.2 Part B - 10%
When one or more ply fails, using Ply by Ply Failure method calculate the following:
1. FoS of each remaining ply and the whole laminate based on Interactive Tensor Polynomial
Theory - Tsai-Wu Criterion
2. Continue this procedure until the catastrophic failure (automated process in excel)
2.3 Part C- 5%
Calculate buckling loads under various loads and boundary conditions.
2.4 Deliverables
A spreadsheet for the given task labelled with your name and student numbers and a clear description (within the spreadsheet) on how it works.
Important Note: This spreadsheet is essential for Task 2.
3 Task 2- Design and analysis of a composite pressure vessel 65%
3.1 Introduction- filament winding
Filament winding is used for the manufacture of parts with high fibre volume fractions and controlled fibre orientation. Fibre tows are immersed in a resin bath where they are coated with low or medium molecular weight reactants. The impregnated tows are then literally wound around a mandrel (mould core) in a controlled pattern to form the shape of the part. After winding, the resin is then cured, typically using heat. The mould core may be removed or may be left as an integral component of the part.
The filament winding process was originally invented to produce missile casings, nose cones and fuselage structures, but with the passage of time industries other than defence and aerospace have discovered the strength and versatility of filament winding. Examples of products created using the process of filament winding include:
• Tubes
• Transmission poles
• Aircraft fuselages
• Gas, water, or tanks
• Cement Mixers
• Pipes
3.2 Brief
Your task is to use your laminate design spreadsheets and the Abaqus ® finite element analysis software package to design a laminate layout for a pressure vessel as shown in Figure 2. The pressure vessel is made of ONLY laminate composites. It is subjected to an internal pressure of 55 bar. Your final design must have a FoS = 2.5.
Figure 2: General layout of a composite pressure vessel subjected to internal pressure
The pressure vessel is supported by two concrete supports as shown in Figure 2. The concrete supports are assumed to be rigid compared to the pressure vessel. The environmental effects of moisture maybe assumed to be negligible.
There are two inlets on each spherical end cap of the pressure vessel and there are two outlets on the top and bottom of cylindrical part as presented inFigure 2throughFigure 3. Diameters of inlets and outlets are 60 mm.
Dimensions of the pressure vessel are given in Figure 3andTable 2.
Figure 3: Geometrical dimensions of the pressure vessel
Table 2: Dimensions for the inner radius and position of supports
Group Number
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R
(mm)
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D
(mm)
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1
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375
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1600
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2
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395
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1700
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3
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370
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1600
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4
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380
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1700
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5
|
360
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1600
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6
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385
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1700
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7
|
365
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1600
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8
|
420
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1700
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9
|
405
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1600
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10
|
415
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1700
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Material properties for the lamina in the principal directions are given inTable 3.
Table 3: Lamina’s properties
E11
|
Longitudinal modulus of elasticity (Mpa)
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110,000
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E22
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Transverse modulus of elasticity (Mpa)
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7,500
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G12
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In-plane shear modulus (Mpa)
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5,000
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Xt
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Tensile strength of ply in longitudinal direction (Mpa)
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1,950
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Xc
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Compressive strength of ply in longitudinal direction (Mpa)
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1,450
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Yt
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Tensile strength of ply in transverse direction (Mpa)
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100
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Yc
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Compressive strength of ply in transverse direction (Mpa)
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200
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S
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In-plane shear strength (Mpa)
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160
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P
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Density (kg/m3 )
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1,350
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θ12
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Poisson's ratio in plane 1-2
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0.3
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α1
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Longitudinal coefficient of thermal expansion (μE/℃)
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13
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α2
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Transverse coefficient of thermal expansion (μE/℃)
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35
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3.3 Procedure
3.3.1 Engineering analysis of the pressure vessel
1. Research on filament winding method (to determine the limitation of this method and
preferable angles of fibres etc.).
2. Use the theory of pressure vessels (without consideration of the pressure vessel’s weight) to determine the applied longitudinal and hoop forces per unit length (Nx , Ny , Nxy , …).
3. Use your spreadsheet to determine the best layout for the applied forces- using Solver® will help you significantly.
4. Use your theoretical laminate layout from step 3 to analyse the pressure vessel using Abaqus® .
5. Perform. a mesh study to determine the optimum size and shape of mesh.
6. Reduce weights by adding patches around the holes instead of making the whole pressure vessel thicker.
7. If your FoS is within limit goto step 8 otherwise change the thickness or angle of fibres or
size or orientation of patches to achieve the given FoS.
3.3.2 Advanced Analysis
8. Investigate on the design and analysis of inlet and outlets and how this affects the FoS.
9. Investigate if this vessel is suitable to carry liquid (density 1000 kg/m3 ) in addition to the given pressure and its weight. Ifnot, change the design to have a FoS of 2.5.
10. Investigation on environmental effect (when temperature changes ΔT = 50℃) on FoS in addition to the given pressure, weight of liquid and vessel. If not, change the design to have a FoS of 2.5.
Note 1:
You need to document every step of your work. Remember that ONLY your report will be marked.
Note 2:
The output of this coursework will be a report in the style of a 10-page conference paper. Please use the provided template (Manuscript_template)