Author:
Wang X. Q.,Mignolet Marc P.
Publisher
Springer International Publishing
Reference8 articles.
1. Matney, A., Mignolet, M.P., Culler, A.J., McNamara, J.J., Spottswood, S.M.: Panel response prediction through reduced order models with application to hypersonic aircraft. In: Proceedings of the AIAA Science and Technology Forum and Exposition (SciTech2015), Orlando, FL, 5–9 Jan 2015, AIAA Paper AIAA 2015-1630
2. Matney, A., Perez, R., Mignolet, M.P.: Nonlinear unsteady thermoelastodynamic response of a panel subjected to an oscillating flux by reduced order models. In: Proceedings of the 52nd structures, structural dynamics and materials conference, 4–7 Apr 2011, Denver, Colorado, AIAA 2011-2016
3. Perez, R., Wang, X.Q., Mignolet, M.P.: Steady and unsteady nonlinear thermoelastodynamic response of panels by reduced order models. In: Proceedings of the 51st structures, structural dynamics, and materials conference, Orlando, FL, 12–15 Apr 2010, Paper AIAA-2010-2724
4. Gogulapati, A., Deshmukh, R., Crowell, A.R., McNamara, J.J., Vyas, V., Wang, X.Q., Mignolet, M., Beberniss, T., Spottswood, S.M., Eason, T.G.: Response of a panel to shock impingement: modeling and comparison with experiments. In: Proceedings of the AIAA Science and Technology Forum and Exposition (SciTech2014), National Harbor, MD, 13–17 Jan 2014, AIAA Paper AIAA 2014-0148
5. Gogulapati, A., Brouwer, K., Wang, X.Q., Murthy, R., McNamara, J.J., Mignolet, M.P.: Full and reduced order aerothermoelastic modeling of built-up aerospace panels in high-speed flows. In: Proceedings of the AIAA Science and Technology Forum and Exposition (SciTech2017), Dallas, TX, 9–13 Jan 2017, Paper AIAA 2017-0180