Aerosandbox

- Verified compatibility with NumPy 2.0.0+; version pin removed.
- Converted formatting to Black, for improved readability.
- Fixed a bunch of minor things using Ruff; removed dead code branches.

- Improvements to AeroSandbox plotting tools (`aerosandbox.tools.pretty_plots`)
- New features in AeroSandbox profiling tools (`aerosandbox.tools.code_benchmarking`)
- In tutorials, added new validation studies for aerodynamics solvers including wind tunnel data

- Fixed a bug in `aerosandbox.numpy.gradient` which resulted in inconsistent answers with `numpy.gradient` (dropped an argument). Added fix for the `period` argument.
- Adds a new tutorial on visualizing flight test data.
- Adds a new tutorial on aircraft noise impact minimization.
- Improved accuracy of transonic modeling with `asb.Airfoil.get_aero_from_neuralfoil()` based on correlation to full-potential and RANS solutions.
- Adds `softmax_scalefree` and `softmin_scalefree` as new surrogate modeling tools. Similar to softmax and softmin, but with a scale dependent on arguments.
- Adds in ability to do `.leading_edge_radius()` calculations in `asb.Airfoil` and `asb.KulfanAirfoil`, which can be used during optimization to prevent sharp leading edges from forming.
- Adds `softplus` and `swish` functions to support neural surrogate modeling.
- Adds preparations for NumPy 2.0 by fixing soon-to-be-deprecated calls.

- Synchronized update: ASB 4.2.3 and NeuralFoil 0.2.0.

- Added Python 3.12 support, after completing investigation of small floating-point math differences between Python 3.11 and 3.12 (caused by backend changes in NumPy 1.24.3 and 1.25.0).
- Updated version pins in `requirements.txt` to match those used in local pre-commit testing.
- Breaking change from 4.2.1: in `asb.XFoil`, to access boundary layer data (new feature from 4.2.1), give `include_bl_data=True` in the `asb.XFoil` constructor rather than in `asb.XFoil.alpha()`.
- In `asb.XFoil`, added more aggressive suppression of pop-up window generation from X11, allowing it to run in the background more reliably.
- Increased the default `asb.XFoil` paneling resolution to 320 points when `xfoil_repanel=True` is given.
- Fixed gimbal lock singularity issues in the solar energy library (`aerosandbox.library.power_solar`), which could cause optimization to fail when the sun is directly overhead.

- Added ability to extract boundary layer data from XFoil via the `asb.XFoil` interface. See `asb.XFoil.alpha(alpha, include_bl_data=True)` for details. This is useful for boundary layer analysis, especially for high-lift devices.
- Added geometry export capabilities to OpenVSP using the *.vspscript interface. Accessible via `asb.Airplane.export_OpenVSP_vspscript(filename="/path/to/my/file.vspscript")`. To import into OpenVSP, use this function to generate a VSPscript file, and then import it via File -> Run Script... in OpenVSP.
- Overhaul of the airfoil database at `aerosandbox.geometry.airfoil.airfoil_database`. This includes the addition of around 500 new high-quality airfoils, the removal of around 15 exceptionally-low-quality airfoils from the UIUC database, the correction of some airfoil coordinates for transcription errors, and fixes for file encodings that caused errors on Linux.