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lines changed Original file line number Diff line number Diff line change @@ -14,11 +14,12 @@ This project is based on version 1.0 of the Python project [Vortex-Step-Method](
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1515## VortexStepMethod v1.1.0 2025-03-04
1616### Added
17- - Dynamically change segments #19
18- - Add rotational velocities #49
17+ - Dynamically deform the KiteWing by twisting the left side and right side, and deforming the trailing edges using deform! #19
18+ - Set turn rate ` omega = [omega_x, omega_y, omega_z] ` in kite body frame using set_va! #49
1919- Add moment coefficient calculations around specified point #17
20- - Add moment distribution around user-defined point #90
20+ - Add moment distribution of the moment around the local panel y-axes around user-defined points on the panels #90
2121- Add function solve!() which returns a ` VSMSolution ` struct #87
22+ - Add the option to remove the NaNs in ` aero_data ` vectors or matrices #98
2223### Changed
23- - Add origin argument to Wing and KiteWing constructor #66
24+ - Add origin argument to BodyAerodynamics constructor #66
2425- Improve documentation
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