An Integrated Aerothermoelastic Analysis Framework for Predicting the Response of Composite Panels
Author:
Affiliation:
1. University of Michigan, Ann Arbor
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-1090
Reference54 articles.
1. Aeroelastic and Aerothermoelastic Analysis in Hypersonic Flow: Past, Present, and Future
2. Loosely Coupled Time-Marching of Fluid-Thermal-Structural Interactions with Time-Accurate CFD
3. Partitioned analysis of coupled mechanical systems
4. Provably second-order time-accurate loosely-coupled solution algorithms for transient nonlinear computational aeroelasticity
5. Impact of Fluid-Thermal-Structural Coupling on Response Prediction of Hypersonic Skin Panels
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