Thermal modal analysis of hypersonic composite wing on transient aerodynamic heating
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DOI: 10.1038/s41598-024-61900-y
Abstract: Considering the influence of thermal stress and material property variations, this study employs the Navier–Stokes equations and Fourier heat conduction law to establish a semi-implicit time-domain numerical analysis method for hypersonic aerothermal-structural coupling. Study the… read more here.
Keywords: analysis hypersonic; aerodynamic heating; thermal modal; modal analysis ... See more keywords