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Rouma Alexandre
Rotare
Commits
e464bbe5
Verified
Commit
e464bbe5
authored
1 year ago
by
Thomas Lambert
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doc(update): complete changelog and release
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CHANGELOG.md
+23
-1
23 additions, 1 deletion
CHANGELOG.md
RELEASE.md
+3
-2
3 additions, 2 deletions
RELEASE.md
src/configs/template.m
+3
-3
3 additions, 3 deletions
src/configs/template.m
with
29 additions
and
6 deletions
CHANGELOG.md
+
23
−
1
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e464bbe5
...
@@ -17,6 +17,27 @@ to [Semantic Versioning][sem_ver].
...
@@ -17,6 +17,27 @@ to [Semantic Versioning][sem_ver].
### Fixed
### 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
## [0.1.2] - 2023-04-28
### Changed
### Changed
...
@@ -75,7 +96,8 @@ _Initial commit_: single rotor in hover/axial flows
...
@@ -75,7 +96,8 @@ _Initial commit_: single rotor in hover/axial flows
[
sem_ver
]:
<
https://semver.org/spec/v2.0.0.html
>
[
sem_ver
]:
<
https://semver.org/spec/v2.0.0.html
>
[
keep_chglog
]:
<
https://keepachangelog.com/en/1.0.0/
>
[
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
[
0.1.2
]:
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
[
0.1.1
]:
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
[
0.1.0
]:
https://gitlab.uliege.be/rotare/rotare/compare/0.0.1...0.1.0
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RELEASE.md
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@@ -10,5 +10,6 @@ automatically generated and do not contain all dependencies.
...
@@ -10,5 +10,6 @@ automatically generated and do not contain all dependencies.
This release features:
This release features:
-
Minor bug fixes for the calculation of polars
-
Functions to plot the velocity triangles
-
Minor tweaks of default values
-
Simpler interface to get the advance ratio
-
**BREAKING**
Output results as a separate object
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src/configs/template.m
+
3
−
3
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...
@@ -83,10 +83,10 @@ Sim.Misc.appli = 'heli'; % Type of application ('helicopter', 'propeller', 'win
...
@@ -83,10 +83,10 @@ Sim.Misc.appli = 'heli'; % Type of application ('helicopter', 'propeller', 'win
% ==================================================================================================
% ==================================================================================================
% Solvers
% Solvers
Mod
.
solvers
=
'
stahlhut
'
;
% BEMT Solver ('leishman', 'indfact', 'indvel', 'stahlhut', 'all')
Mod
.
solvers
=
'
all
'
;
% BEMT Solver ('leishman', 'indfact', 'indvel', 'stahlhut', 'all')
% Extensions/corrections
% 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
% Numerical parameters
Mod
.
Num
.
convCrit
=
1e-4
;
% Convergence criterion value,
Mod
.
Num
.
convCrit
=
1e-4
;
% Convergence criterion value,
...
@@ -110,7 +110,7 @@ Flow.fluid = 'air'; % Fluid ('air', 'seawater', 'freshwater')
...
@@ -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
% 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.
% 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
.
collective
=
[
2
,
5
,
8
];
% Collective pitch, [deg]
Op
.
rpm
=
[
1000
,
1300
];
% Rotor angular velocity, [RPM]
Op
.
rpm
=
[
1000
,
1300
];
% Rotor angular velocity, [RPM]
Op
.
altitude
=
0
;
% Flight altitude (only used if Flow.fluid = 'air'), [m]
Op
.
altitude
=
0
;
% Flight altitude (only used if Flow.fluid = 'air'), [m]
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