From 2c19403f1e96d1ad22719caa7d70be1f7b311dc0 Mon Sep 17 00:00:00 2001 From: =?UTF-8?q?R=C3=A9gis=20LEBRUN?= Date: Sat, 6 Apr 2024 08:43:46 +0200 Subject: [PATCH] Update python/doc/usecases/use_case_stiffened_panel.rst Co-authored-by: Michael Baudin <31351465+mbaudin47@users.noreply.github.com> --- python/doc/usecases/use_case_stiffened_panel.rst | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/python/doc/usecases/use_case_stiffened_panel.rst b/python/doc/usecases/use_case_stiffened_panel.rst index 151949bb343..b4ee384f2c6 100644 --- a/python/doc/usecases/use_case_stiffened_panel.rst +++ b/python/doc/usecases/use_case_stiffened_panel.rst @@ -65,7 +65,7 @@ We assume that the input variables are independent except the :math:`f_1` and :math:`f_2` for which we measure a Spearman correlation of :math:`\rho^S_{12}=-0.8`, modelled using a :class:`~openturns.NormalCopula`. -The critical load :math:`(\tau_{xy})_{cr}` of a stiffened panel subject to shear load is given by +The critical load :math:`(\tau_{xy})_{cr}` of a stiffened panel subject to shear load is: .. math:: (\tau_{xy})_{cr}=k_{xy}\frac{\pi^2D}{b_0^2t_s}