@inproceedings{3b1559004986407b9820cd761d312df6,
title = "Response of a panel to shock impingement: Modeling and comparison with experiments - part 2",
abstract = "This paper describes an on-going effort towards the prediction of structural responses to shock impingements. This work is an extension of a previous effort, where the focus is on several potential sources of discrepancy between the experiments and simulations. In particular, the thermal state of the panel is examined by incorporating a nonlinear thermal solver into the fluid-structural interaction framework. Additionally, attention is given to the turbulent boundary layer loads, the potential role of shock unsteadiness on panel responses, and discrepancies in free vibration frequencies. Improved correlation with experimental results are found when including both thermal analysis and shock unsteadiness.",
author = "A. Gogulapati and R. Deshmukh and McNamara, {J. J.} and V. Vyas and Wang, {X. Q.} and M. Mignolet and T. Beberniss and Spottswood, {S. M.} and Eason, {T. G.}",
note = "Publisher Copyright: {\textcopyright} 2015, American Institute of Aeronautics and Astronautics Inc. All rights reserved.; 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 2015 ; Conference date: 05-01-2015 Through 09-01-2015",
year = "2015",
doi = "10.2514/6.2015-0685",
language = "English (US)",
series = "56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
booktitle = "56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference",
}