Answer:
The plane with aluminium can lift more mass of passangers than the plane of steel.
Explanation:
The total mass the airplane canc lift is:
[tex]m_{tot}=m_{fuselage}+m_{passangers}[/tex]
For aluminium:
[tex]m_{tot}=m_{fus-Al}+m_{pas-Al}[/tex]
[tex]m_{fus-Al}=\delta _{Al}*V_{fuselage}[/tex]
and
[tex]V_{fuselage}=\frac{\pi *L}{4}*[D^2-(D-e)^2][/tex]
where:
[tex]m_{tot}=\delta _{Al}*\frac{\pi *L}{4}*[D^2-(D-e)^2]+m_{pas-Al}[/tex]
For steel (same procedure):
[tex]m_{tot}=\delta _{Steel}*\frac{\pi *L}{4}*[D^2-(D-e)^2]+m_{pas-Steel[/tex]
Knowing that the total mass the airplane can lift is constant and that aluminum has a lower density than the steel, we can afirm that the plane with aluminium can lift more mass of passangers.
Also you can estimate an average weight of passanger to estimate a number of passangers it can lift.