Aluminum–lithium (Al–Li) alloys have been developed by the aircraft industry to reduce the weight and improve the performance of its aircraft. A commercial aircraft skin material having a density of 2.14 g/cm3 is desired. Compute the concentration of Li (in wt%) that is required. The densities of aluminum and lithium are 2.71 and 0.534 g/cm3, respectively.

Respuesta :

Answer:

6.54% is the required concentration of lithium in an alloy (Al–Li).

Explanation:

Suppose 100 grams of an alloy of aluminium and lithium.

Density of an alloy = d  [tex]2.14 g/cm^3[/tex]

Volume of an alloy = V

[tex]V=\frac{100 g}{2.14 g/cm^3}=46.73 cm^3[/tex]

Volume of aluminum = [tex]v_1[/tex]

Mass of aluminum = x

Density of aluminum = [tex]d_1=2.71 g/cm^3[/tex]

[tex]v_1=\frac{x}{d_1}[/tex]

Volume of lithium = [tex]v_2[/tex]

Mass of lithium = y

Density of lithium= [tex]d_2=0.534 g/cm^3[/tex]

[tex]v_2=\frac{y}{d_2}[/tex]

[tex]x+y=100[/tex] ..[1]

[tex]v_1+v_2=V[/tex]

[tex]\frac{x}{d_1}+\frac{y}{d_2}=46.73 cm^3[/tex]

[tex]\frac{x}{2.71}+\frac{y}{0.534}=46.73[/tex]..[2]

Solving [1] and [2] :

we get :

x = 93.46 g

y = 6.54 g

Concentration of Li (in wt%) that is required:

[tex]Li\%=\frac{6.54 g}{100 g}\times 100=6.54\%[/tex]