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peterdsharpe · Oct 6, 2023 · 5c3a869 · 5c3a869
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diff --git a/CHANGELOG.md b/CHANGELOG.md
@@ -34,12 +34,14 @@ Also, for at least one version before a breaking change, AeroSandbox development
 
 # In-progress (develop) version
 
-- Added improvements to `asb.LiftingLine` to ensure mixed-backend compatibility.
-
 -----
 
 # Latest (master / release), and previous versions
 
+#### 4.1.5
+
+- Added improvements to `asb.LiftingLine` to ensure mixed-backend compatibility.
+
 #### 4.1.4
 
 - Public release of `asb.NonlinearLiftingLine`, which is a new 3D aerodynamics analysis method implemented by Yashil Choony (@yashil99) at Politecnico di Milano. It is implicitly solved (i.e., by iteration), subclassing `asb.ImplicitAnalysis`. This is a nonlinear lifting line theory method (with sweep and dihedral accounting), where the CL(alpha) function used to drive the nonlinear closure loop is taken from NeuralFoil. Fuselage influences can be optionally handled using a source-line (i.e. nonlifting) method. Preliminary testing on full-aircraft configurations indicates good agreement with other solvers, but production use should likely wait until more testing is performed in future versions.

diff --git a/aerosandbox/__init__.py b/aerosandbox/__init__.py
@@ -14,7 +14,7 @@
 from aerosandbox.propulsion import *
 from aerosandbox.structures import *
 
-__version__ = "4.1.4"
+__version__ = "4.1.5"
 
 
 def docs():