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Tutorial 3: Derivation of performance indices 1. Performance index for stiff and light flat panel In this example we are free to alter beam thickness (t) to attain desired stiffness Panel thickness t is a free variable a) By deriving an expression for the mass of the panel, justify a performance index for specific stiffness of the panel, based on free variable being panel thickness (t) b) Perform material selection using performance index for calculated in a) for maximising specific stiffness. Yield strength > 30MPa Fracture toughness > 5MPa.m 0.5 .Want to minimise cost S= 48 EI L 3

CES Tutorial 3 Derivation of Performance Indices (Feb 2014)

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Tutorial 3: Derivation of performance indices

1. Performance index for stiff and light flat panel

In this example we are free to alter beam thickness (t) to attain desired stiffnessPanel thickness t is a free variable

a) By deriving an expression for the mass of the panel, justify a performance index for specific stiffness of the panel, based on free variable being panel thickness (t)b) Perform material selection using performance index for calculated in a) for maximising specific stiffness. Yield strength > 30MPa Fracture toughness >5MPa.m0.5.Want to minimise cost

2. Performance index for strong and light flat panel

Figure A Panel in three point bending

The situation shown in the figure A shows a panel loaded in three point bending; load F being in the middle of the loading span (L). The width (w) of the panel is fixed, the thickness (t) is the design free variable

a) Derive an expression for the mass of the panel that is independent of the design free variable (thickness t). The derived expression containing a material performance index for specific strength. The loading is static and the panel must remain completely elastic.

b) State the final material performance index in a form such that it is to be maximised to allow ranking of candidate materials for this

c) Table 1 shows properties for five candidate materials, for each material calculate the material performance index for specific strength and hence justify selection of the optimum material based on highest value of the performance index (independent of material cost constraints)

d) Modify the performance index to take into account material cost (per Kg) and recalculate modified performance index for each material so as to justify the most cost effective material for the application Where M= bending momentI= second moment of area= stress at distance y from panel neutral axis= density

Mg wrought(AZ31)Mg cast(AZ91)Al 7075 T6Ti-6Al-4VCFRP (quasi-isotropic)

Yield strength(x 106 N.m-2)155145450900550

Density(Kg.m-3)17801800280044301575

Material cost (/Kg)2.252.221835

Table 1: Material properties of candidate materials

3. Material selection: Oars

Derive a material performance index to select materials for light stiff oars.

Function: Light & stiff beam

Objective: Minimise mass, maximise stiffness

Constraintsa) Length (L) specifiedb) Bending stiffness (S) specifiedc) Minimum Toughness specified d) Material cost, CM < 50/Kg

Circular cross- section: free variable: Radius (R)Assume loading in bending, maximise specific stiffness

Given

Mass, m = A.L. = .R2. L.

Stiffness of C = Loading configuration constant = 24 for this case E= Material elastic modulus, I = 2nd Moment of area

For solid cylinder, 2nd Moment of area

Using the performance index you have derived for a light stiff oar along with the minimum toughness constraint to plot a selection graph (use advanced function when plotting graph to plot relevant functions on each axis.

Then assess the best four materials for price