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An Aircraft Design Toolbox

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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...

enhancement

# 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 is a neat script I used during my thesis. A few universities who reached out to me for eVTOL design also found it useful. It basically ensures that the...

Here are some updates you should consider for the following plugins: Change collections library: /trunk/SUAVE/Plugins/pint/compat.py:from collections import MutableMapping to `collections.abc` Also in: `/trunk/SUAVE/Plugins/pint/quantity.py` Cheers

[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)

I guess this should be `** (3/4)` and not `** 3/4`? https://github.com/suavecode/SUAVE/blob/dc46e127f04ce34733bd952d429f50e101fb3ad1/trunk/SUAVE/Methods/Noise/Fidelity_One/Propeller/compute_broadband_noise.py#:~:text=%2B%200.5)-,**3/4,-))/( ![image](https://user-images.githubusercontent.com/90248888/222458614-af5b383b-96c5-454f-b2bf-5d803a021ea3.png)

This PR adds a new mission segment for eVTOL transition. This is a linear acceleration, constant pitch rate, constant altitude segment. The assumption of linear numerics is required to solve...

# 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...

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