From d37a3ab0cb9aab00dde507cc3e1f8437a9bf6f49 Mon Sep 17 00:00:00 2001 From: MateusStano Date: Wed, 18 Sep 2024 01:40:42 +0200 Subject: [PATCH] MNT: lint --- rocketpy/rocket/aero_surface/fins/free_form_fins.py | 7 +++++-- 1 file changed, 5 insertions(+), 2 deletions(-) diff --git a/rocketpy/rocket/aero_surface/fins/free_form_fins.py b/rocketpy/rocket/aero_surface/fins/free_form_fins.py index 3e6ac2c95..a274495ba 100644 --- a/rocketpy/rocket/aero_surface/fins/free_form_fins.py +++ b/rocketpy/rocket/aero_surface/fins/free_form_fins.py @@ -201,13 +201,16 @@ def evaluate_center_of_pressure(self): def evaluate_geometrical_parameters(self): # pylint: disable=too-many-statements """ Calculates and saves the fin set's geometrical parameters such as the - fin area, aspect ratio, and parameters related to roll movement. This method - uses similar calculations to those in OpenRocket for free-form fin shapes. + fin area, aspect ratio, and parameters related to roll movement. This + method uses the same calculations to those in OpenRocket for free-form + fin shapes. Returns ------- None """ + # pylint: disable=invalid-name + # pylint: disable=too-many-locals # Calculate the fin area (Af) using the Shoelace theorem (polygon area formula) Af = 0 for i in range(len(self.shape_points) - 1):