v1.1.0

VortexStepMethod v1.1.0

Diff since v1.0.1

Added

• Dynamically deform the KiteWing by twisting the left side and right side, and deforming the trailing edges using deform!
• Set turn rate omega = [omega_x, omega_y, omega_z] in kite body frame using set_va!
• Add moment coefficient calculations around specified point to solve
• Add moment distribution of the moment around the local panel y-axes around user-defined points on the panels to solve!
• Add function solve!() which returns a VSMSolution struct
• Add the option to remove the NaNs in aero_data vectors or matrices using the remove_nan keyword in the Wing and KiteWing constructors

Changed

• Add origin argument to BodyAerodynamics constructor
• Improve documentation

Merged pull requests:

• Update docstring of Solver, use @with_kw (#81) (@ufechner7)
• Refactor Section, use @with_kw; refactor Wing (#82) (@ufechner7)
• add type AeroData (#86) (@ufechner7)
• Add solve!(res::Results, ...) (#88) (@ufechner7)
• Add trailing edge angle beta and deform (#89) (@1-Bart-1)
• Moment distribution (#95) (@1-Bart-1)
• Add origin parameter to BodyAerodynamics constructor (#96) (@1-Bart-1)
• Add the option to remove nans (#98) (@1-Bart-1)

Closed issues:

• Register and release version 1.0.1 (#13)
• Dynamically change segments. (#19)
• Don't assume constant radius on KiteWing creation (#42)
• Add origin argument to Wing and KiteWing constructor (#66)
• Write announcement for the new package, version 1.0.1 (#68)
• Add type AeroData (#85)
• Add a Results struct (#87)
• Add moment distribution around user-defined point (#90)
• Remove NaNs from XFoil polar matrices so the solver doesn't crash (#97)