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improve news
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NEWS.md

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@@ -16,10 +16,10 @@ This project is based on version 1.0 of the Python project [Vortex-Step-Method](
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### Added
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- Dynamically deform the KiteWing by twisting the left side and right side, and deforming the trailing edges using deform! #19
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- Set turn rate `omega = [omega_x, omega_y, omega_z]` in kite body frame using set_va! #49
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- Add moment coefficient calculations around specified point #17
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- Add moment distribution of the moment around the local panel y-axes around user-defined points on the panels #90
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- Add function solve!() which returns a `VSMSolution` struct #87
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- Add the option to remove the NaNs in `aero_data` vectors or matrices #98
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- Add moment coefficient calculations around specified point to `solve` #17
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- Add moment distribution of the moment around the local panel y-axes around user-defined points on the panels to `solve!` #90
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- Add function `solve!()` which returns a `VSMSolution` struct #87
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- Add the option to remove the NaNs in `aero_data` vectors or matrices using the `remove_nan` keyword in the `Wing` and `KiteWing` constructors #98
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### Changed
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- Add origin argument to BodyAerodynamics constructor #66
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- Add origin argument to `BodyAerodynamics` constructor #66
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- Improve documentation

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