Consider the plate shown below that is supported at its ends and subjected to
a force \(F\) that is uniformly distributed over the upper face as indicated.
The deflection \(\delta\) at the \(L / 2\) position is given by the expression
$$\delta=\frac{5 F L^{3}}{32 E w t^{3}}$$ Furthermore, the tensile stress at
the underside and also at the \(L / 2\) location is equal to $$\sigma=\frac{3 F
L}{4 w t^{2}}$$ (a) Derive stiffness and strength performance index
expressions analogous to Equations 22.9 and 22.11 for this plate (Hint. solve
for \(t\) in these two equations, and then substitute the resulting expressions
into the mass equation, as expressed in terms of density and plate
dimensions.) (b) From the properties database in Appendix \(\mathrm{B},\) select
those metal alloys with stiffness performance indices greater than 1.40 (for
\(E\) and \(\rho\) in units of \(\mathrm{GPa}\) and \(\mathrm{g} / \mathrm{cm}^{3}\)
respectively). (c) Also using the cost database (Appendix
C), conduct a cost analysis in the same manner as Section \(22.2 .\) Relative to
this analysis and that in part b, which alloy would you select on a stiffness-
per-mass basis?
(d) Now select those metal alloys having strength performance indices greater
than 5.0 (for \(\sigma_{y}\) and \(\rho\) in units of \(\mathrm{MPa}\) and
\(\mathrm{g} / \mathrm{cm}^{3}\) respectively \(),\) and rank them from highest to
lowest \(P\).(e) And, using the cost database, rank the materials in part d from
least to most costly. Relative to this analysis and that in part d, which
alloy would you select on a strength-per-mass basis?
(f) Which material would you select if both stiffness and strength are to be
considered relative to this application? Justify your choice.