Solution de référence ===================== Méthode de calcul ------------------ Solution numérique [:ref:`bib1 `] : valeurs du paramètre de pilotage (donc de la force :math:`P` ) en fonction du temps (donc du déplacement :math:`\mathit{Uz}` du point :math:`A` ). Grandeurs et résultats de référence ----------------------------------- .. code-block:: text Coefficient de pilotage (coefficient Multiplicateur de la force appliquée) en fonction du déplacement :math:`\mathrm{Uz}`du point :math:`A`. .. code-block:: text Résultats de référence obtenus par une modélisation en 16x1x1 éléments coque :math:`\mathrm{S4R}`d’Abaqus. .. csv-table:: ":math:`P/{P}_{max}`", ":math:`-{U}_{x}(m)`", ":math:`{U}_{z}(m)`", ":math:`P/{P}_{\max}`", ":math:`-{U}_{x}(m)`", ":math:`{U}_{z}(m)`", ":math:`P/{P}_{\max}`", ":math:`-{U}_{x}(m)`", ":math:`{U}_{z}(m)`" "0.05", "0,026", "0,663", "0,4", "1,184", "4,292", "0,75", "2,541", "6,031" "0.1", "0,103", "1,309", "0,45", "1,396", "4,631", "0,8", "2,705", "6,190" "0.15", "0,224", "1,922", "0,5", "1,604", "4,933", "0,85", "2,861", "6,335" "0.2", "0,381", "2,493", "0,55", "1,807", "5,202", "0,9", "3,01", "6,467" "0.25", "0,563", "3,015", "0,6", "2,002", "5,444", "0,95", "3,151", "6,588" "0.3", "0,763", "3,488", "0,65", "2,190", "5,660", "1", "3,286", "6,698" "0.35", "0,971", "3,912", "0,7", "2,370", "5.855", "", "", "" Incertitudes sur la solution ---------------------------- Sans objet Références bibliographiques --------------------------- .. _Ref208649747: 1. Sze K.Y, Liu X.H, and Lo S.H. Popular benchmark problems for geometric nonlinear analysis of shells. *Finite Elements in Analysis and Design,* Volume 40, Issue 11, Pages 1551-156, 2004.