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lines changed Original file line number Diff line number Diff line change @@ -16,10 +16,10 @@ This project is based on version 1.0 of the Python project [Vortex-Step-Method](
1616### Added
1717- Dynamically deform the KiteWing by twisting the left side and right side, and deforming the trailing edges using deform! #19
1818- Set turn rate ` omega = [omega_x, omega_y, omega_z] ` in kite body frame using set_va! #49
19- - Add moment coefficient calculations around specified point #17
20- - Add moment distribution of the moment around the local panel y-axes around user-defined points on the panels #90
21- - Add function solve!() which returns a ` VSMSolution ` struct #87
22- - Add the option to remove the NaNs in ` aero_data ` vectors or matrices #98
19+ - Add moment coefficient calculations around specified point to ` solve ` #17
20+ - Add moment distribution of the moment around the local panel y-axes around user-defined points on the panels to ` solve! ` #90
21+ - Add function ` solve!() ` which returns a ` VSMSolution ` struct #87
22+ - 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
2323### Changed
24- - Add origin argument to BodyAerodynamics constructor #66
24+ - Add origin argument to ` BodyAerodynamics ` constructor #66
2525- Improve documentation
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