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NEWS.md

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@@ -14,11 +14,12 @@ This project is based on version 1.0 of the Python project [Vortex-Step-Method](
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## VortexStepMethod v1.1.0 2025-03-04
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### Added
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- Dynamically change segments #19
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- Add rotational velocities #49
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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 around user-defined point #90
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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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### Changed
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- Add origin argument to Wing and KiteWing constructor #66
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- Add origin argument to BodyAerodynamics constructor #66
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- Improve documentation

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