Consider the Boeing $747-100$ in the mid$-$altitude cruise configuration Case II as described in

Appendix E of Etkin and Reid. Based on the data provided in Table E$.3$ and Table E$\mathrm{.}1,$

estimate values for the lift slope, C$\_($L$\_(\backslash$alpha $)),$ static margin $($h$\_($n$)-$h$),$ and manuever margin $($h$\_($m$)-$h$)$

Note: You can assume C$\_($Z$)$~~$-$C$\_($L$).$

Hint: You will need to find C$\_($m$\_(\backslash$alpha $)),$C$\_($m$\_($q$)),$C$\_($L$\_($q$))$C$\_($L$\_(\backslash$alpha $))$