{"id":2721,"date":"2021-07-12T23:25:35","date_gmt":"2021-07-12T14:25:35","guid":{"rendered":"https:\/\/c-mng.cwh.hokudai.ac.jp\/stl.eng\/Root\/?page_id=2721"},"modified":"2023-11-14T15:04:34","modified_gmt":"2023-11-14T06:04:34","slug":"aerodynamic_instability","status":"publish","type":"page","link":"https:\/\/c-mng.cwh.hokudai.ac.jp\/stl.eng\/Root\/en\/research\/aerodynamic_instability.html","title":{"rendered":"Aerodynamic instability"},"content":{"rendered":"

Aerodynamic instability of capsule with thin and large aeroshell\"\"<\/strong><\/span>
\nA thin, large aeroshell technology has been proposed for an innovative reentry capsule. We are investigating the aerodynamic instability and mitigation methods using a coupled analysis approach.<\/p>\n

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\nFlow field around capsule with thin and large aeroshell (Density distribution).<\/p>\n

Aerodynamic simulation for Hayabusa-type reentry capsule<\/strong><\/span>
\nHayabusa-type sample return capsule (SRC) is a candidate for application in future sample return missions. However, SRC exhibits aerodynamic instability in the transonic region. We are also investigating instability using high-performance computers and computational science approaches to mitigate it.<\/p>\n

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Flow field around Hayabusa SRC at transonic speed.<\/p>\n

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