What is it about?
A simulation method was realized to predict aeroelastic response and characteristic parameters of wing structure. This method was developed base on interaction between Fluent solver and Mechanical APDL solver using a coupling system in ANSYS Workbench. AGARD 445.6 wing model was chose for this developed procedure at high speed.
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This page is a summary of: Research on Simulation and Experiment of Dynamic Aeroelastic Analysis on Wing Structure, Applied Mechanics and Materials, October 2015, Trans Tech Publications,
DOI: 10.4028/www.scientific.net/amm.798.541.
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