{"id":2648,"date":"2021-07-09T19:49:45","date_gmt":"2021-07-09T10:49:45","guid":{"rendered":"https:\/\/c-mng.cwh.hokudai.ac.jp\/stl.eng\/Root\/?page_id=2648"},"modified":"2023-11-14T15:02:48","modified_gmt":"2023-11-14T06:02:48","slug":"fsi","status":"publish","type":"page","link":"https:\/\/c-mng.cwh.hokudai.ac.jp\/stl.eng\/Root\/en\/research\/fsi.html","title":{"rendered":"Fluid-structure interaction"},"content":{"rendered":"

We have investigated the fluid-structure interaction (FSI) using a coupled analysis that combines OpenFOAM–CalculiX and SU2–CalculiX using the coupling library, preCICE<\/a>.<\/p>\n

FSI simulation for inflatable reentry vehicle
\n<\/strong><\/span>A coupled analysis model was developed by comparing the FSI simulation and wind tunnel experiments.<\/p>\n

\"\"\u3000\u3000\u3000\u3000\u3000\"\"\u3000\u3000\u3000\u3000<\/strong>\"\"<\/p>\n

Wind tunnel model\u3000\u00a0 \u00a0Simulation model\u3000\u3000\u3000\u3000\u3000\u00a0 \u00a0 \u00a0 \u00a0 \u00a0 \u00a0 \u00a0 \u3000FSI simulation<\/p>\n

FSI simulation for a thin wing at transonic or supersonic speeds
\n<\/strong><\/span>Limit cycle oscillation of a flat wing was also investigated using an FSI model comprising SU2 and CalculiX with preCICE library. Please refer to the preCICE website
here<\/a>.<\/span>
\n<\/strong><\/span><\/p>\n

Related paper<\/span><\/strong>
\n<\/strong><\/p>\n