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Advanced computational methods are developed to account for the temperature dependence of the properties of structures when performing computations of the structural response, aerodynamic flow, and temperature distribution on components of hypersonic vehicles during a mission.

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This page is a summary of: Nonlinear Reduced Order Modeling of Heated Structures with Temperature-Dependent Properties, AIAA Journal, January 2025, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j064577.
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