Deformation of a Panel in Repeated High Speed Flow Modeled with Creep and Multiplicatively-Decomposed Plasticity
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[1] Assad A. Oberai,et al. Automated Wing Internal Structure Placement Guided by Finite Element Analysis , 2019, AIAA Aviation 2019 Forum.
[2] Assad A. Oberai,et al. Simulation of finite-strain inelastic phenomena governed by creep and plasticity , 2018 .
[3] J. McNamara,et al. Effects of Strain Hardening on Response of Skin Panels in Hypersonic Flow , 2016 .
[4] Laurent Dala,et al. Generalized Formulation and Review of Piston Theory for Airfoils , 2016 .
[5] S. M. Spottswood,et al. A Structures Perspective on the Challenges Associated with Analyzing a Reusable Hypersonic Platform , 2013 .
[6] Jack J. McNamara,et al. Impact of Fluid-Thermal-Structural Coupling on Response Prediction of Hypersonic Skin Panels , 2011 .
[7] Peretz P. Friedmann,et al. Aeroelastic and Aerothermoelastic Analysis in Hypersonic Flow: Past, Present, and Future , 2011 .
[8] Raffaele Savino,et al. Aerothermodynamic Study of Ultrahigh-Temperature Ceramic Winglet for Atmospheric Reentry Test , 2008 .
[9] Chuh Mei,et al. Finite Element Modal Formulation for Hypersonic Panel Flutter Analysis with Thermal Effects , 2003 .
[10] E. Thornton,et al. Coupled flow, thermal, and structural analysis of aerodynamically heated panels , 1986 .