doc(update): complete changelog and release

CHANGELOG.md

@@ -17,6 +17,27 @@ to [Semantic Versioning][sem_ver].
 
 ### Fixed
 
+## [0.1.3] - 2023-05-25
+
+### Added
+
+- Possibility to plot the velocity triangles along the blade
+- Simpler interface to get rotor advance ratio
+- **BREAKING** Result class to gather all results
+
+### Changed
+
+- Adjustments to blade plotting
+- Minor equation rewrite in indvel
+
+### Deprecated
+
+### Removed
+
+### Fixed
+
+- Errors in Knight and Hefner configuration
+
 ## [0.1.2] - 2023-04-28
 
 ### Changed
@@ -75,7 +96,8 @@ _Initial commit_: single rotor in hover/axial flows
 [sem_ver]:<https://semver.org/spec/v2.0.0.html>
 [keep_chglog]: <https://keepachangelog.com/en/1.0.0/>
 
-[Unreleased]: https://gitlab.uliege.be/rotare/rotare/compare/0.1.2...main
+[Unreleased]: https://gitlab.uliege.be/rotare/rotare/compare/0.1.3...main
+[0.1.3]: https://gitlab.uliege.be/rotare/rotare/compare/0.1.2...0.1.3
 [0.1.2]: https://gitlab.uliege.be/rotare/rotare/compare/0.1.1...0.1.2
 [0.1.1]: https://gitlab.uliege.be/rotare/rotare/compare/0.1.0...0.1.1
 [0.1.0]: https://gitlab.uliege.be/rotare/rotare/compare/0.0.1...0.1.0

RELEASE.md

@@ -10,5 +10,6 @@ automatically generated and do not contain all dependencies.
 
 This release features:
 
-- Minor bug fixes for the calculation of polars
-- Minor tweaks of default values
+- Functions to plot the velocity triangles
+- Simpler interface to get the advance ratio
+- **BREAKING** Output results as a separate object

src/configs/template.m

@@ -83,10 +83,10 @@ Sim.Misc.appli  = 'heli'; % Type of application ('helicopter', 'propeller', 'win
 % ==================================================================================================
 
 % Solvers
-Mod.solvers = 'stahlhut';  % BEMT Solver ('leishman', 'indfact', 'indvel', 'stahlhut', 'all')
+Mod.solvers = 'all';  % BEMT Solver ('leishman', 'indfact', 'indvel', 'stahlhut', 'all')
 
 % Extensions/corrections
-Mod.Ext.losses = 'all';    % Include losses using Prandtl formula ('none', 'hub', 'tip', 'both')
+Mod.Ext.losses = 'none';    % Include losses using Prandtl formula ('none', 'hub', 'tip', 'both')
 
 % Numerical parameters
 Mod.Num.convCrit = 1e-4;  % Convergence criterion value,
@@ -110,7 +110,7 @@ Flow.fluid = 'air';  % Fluid ('air', 'seawater', 'freshwater')
 % Note that the code will loop on every combination of these fours. So the total number of
 % simulations can be very large if you want lots of operating points.
 
-Op.speed      = 2:5:12;             % (Axial) Velocity, [m/s]
+Op.speed      = [2, 5];             % (Axial) Velocity, [m/s]
 Op.collective = [2, 5, 8];          % Collective pitch, [deg]
 Op.rpm        = [1000, 1300];  % Rotor angular velocity, [RPM]
 Op.altitude   = 0;                  % Flight altitude (only used if Flow.fluid = 'air'), [m]