Fuselage cannot have z offset in front of the wing/fuselage junction (towards the nose)

[kccwing]

Describe the bug
as described - structural solver nonconvergence observed

To Reproduce
branch dev_fuselage_bug - simple_HALE/generate_hale_nose.py vs simple_HALE/generate_hale_nose_dip.py

Expected behaviour
convergence and time-stepping until completion

Screenshots
|==========|==========|==========|==========|==========|==========|==========|==========|==========|==========|
| iter |alpha[deg]|elev[deg] | thrust | Fx | Fy | Fz | Mx | My | Mz |
|==========|==========|==========|==========|==========|==========|==========|==========|==========|==========|
Residual is: 3.3313240830999096E-006
STOP Static equations did not converge (17235)

System Info (please complete the following information):

• OS: [e.g. CentOS7/MacOS 13.1] HPC
• SHARPy Version - latest

Additional context
prime suspect - CRV in this particular direction? Will do a bit more digging later - just starting this to keep it logged

[kccwing]

dev_fuselage_bug