{"id":3065,"date":"2023-03-14T15:35:24","date_gmt":"2023-03-14T06:35:24","guid":{"rendered":"https:\/\/c-mng.cwh.hokudai.ac.jp\/stl.eng\/Root\/?p=3065"},"modified":"2023-03-14T15:36:25","modified_gmt":"2023-03-14T06:36:25","slug":"news-20230314_en","status":"publish","type":"post","link":"https:\/\/c-mng.cwh.hokudai.ac.jp\/stl.eng\/Root\/en\/news\/news-20230314_en.html","title":{"rendered":"Paper published on Aerospace Science and Technology"},"content":{"rendered":"
A paper in which Mr. Sanjoy Kumar Saha is the first author was published in Aerospace Science and Technology. We revealed fluid-structure interaction (FSI) of membrane aeroshell by wind tunnel experiments and numerical simulation based on a partitioned coupling approach. S. K. Saha, J. Tobari, Y. Takahashi, N. Oshima, T. Moriyoshi, K. Yamada, and R. Shibata, \u201cFluid-Structure Interaction Characteristics of Inflatable Reentry Aeroshell at Subsonic Speed\u201d, Aerospace Science and Technology, Vol. 133, 108112, February 2023. DOI: 10.1016\/j.ast.2023.108112.<\/p>\n
\nhttps:\/\/www.sciencedirect.com\/science\/article\/pii\/S1270963823000093<\/a><\/p>\n