Emilio Botero

Feature rotor diff

2

# Pull Request Checklist * Merge in the latest Develop branch changes to your branch * Remove .pyc files from your repository: * Linux/Mac * find . -name *.pyc -delete...

This makes no sense to have the check for battery be aerodynamic in a constant mass vehicle. [See here.](https://github.com/suavecode/SUAVE/blob/develop/regression/scripts/battery/aircraft_discharge_comparisons.py#L86)

Delete this line: https://github.com/suavecode/SUAVE/blob/develop/trunk/SUAVE/Components/Energy/Networks/Solar.py#L242 It's already set above when battery calcs are done.

Throws an error even if flaps are attached

Need some kind of sizing routine.

Would be nice to reimplement methods for breguet range equation, simple rates of climb calculations, and associated weight estimations. For those curious similar files were included in the past: /SUAVE/Trunk/SUAVE/Methods/Performance/cruise_range.py...

[Right here it doesn't take into account the control surfaces as VLM wings.](https://github.com/suavecode/SUAVE/blob/develop/trunk/SUAVE/Analyses/Aerodynamics/Vortex_Lattice.py#L688)

Areas are still present in the network despite nacelle objects being used.

This line doesn't work because of the bnd https://github.com/suavecode/SUAVE/blob/develop/trunk/SUAVE/Methods/Propulsion/electric_motor_sizing.py#L203

Update the docs and website, there are a ton of new options for the VLM for control surfaces.