Thermal flutter prediction at trajectory points of a hypersonic vehicle based on aerothermal synchronization algorithm
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DOI: 10.1016/j.ast.2019.105381
Abstract: Abstract Due to orders of magnitude differences in time scale between structural heat transfer and aeroelastic responses, one-way aerothermal-aeroelastic coupling is adopted to develop a thermal flutter prediction method for a hypersonic vehicle operating along… read more here.
Keywords: trajectory; thermal flutter; hypersonic vehicle; flutter prediction ... See more keywords