Time-adaptive loosely coupled analysis on fluid–thermal–structural behaviors of hypersonic wing structures under sustained aeroheating
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference34 articles.
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2. Multiphysics coupled fluid/thermal/structural simulation for hypersonic reentry vehicles;Tabiei;J. Aerosp. Eng.,2011
3. Studies on fluid-structural coupling for aerothermoelasticity in hypersonic flow;Culler;AIAA J.,2010
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