input file for stab
boeing747
1
7.0        dihedral_wing
6.2        z_wing
23.0       dia_fuse
5500.      sref
33.5       hspan_vtail
14.4       depth_fuse_vtail
36.4       c_vtail_root
11.5       c_vtail_tip
0.25       mach_eo
45.        sweep_vtail_1_4
33.5       sweep_wing_1_2
97.8       hspan_wing
1.11       cl
26.        z_vtail
100.       l_vtail
225.2      length_fuse
4          new
0          nef
8.4        dia_nacelle
1467.      sh
2.3769e-3  rho_eo
1116.4     a_eo
3.7372e-7  mu_eo
15.        dr_max
0.0	   xbar(*) 
27.31	   cbar(**)


(*)  xbar is the longitudinal distance (positive rearward)
     from the coordinate origin (usually the center of
     gravity) to the wing aerodynamic center (ft).

(**) cbar is the mean aerodynamic chord (ft).
