{"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> Aerodynamic simulation for Hayabusa-type reentry capsule<\/strong><\/span> <\/p>\n Flow field around Hayabusa SRC at transonic speed.<\/p>\n Related paper<\/span><\/strong><\/p>\n Aerodynamic instability of capsule with thin and large aeroshell A thin, large aeroshell technology has been p…<\/p>\n","protected":false},"author":2,"featured_media":0,"parent":2646,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"","meta":{"_locale":"en_US","_original_post":"https:\/\/c-mng.cwh.hokudai.ac.jp\/stl.eng\/Root\/?page_id=2474"},"_links":{"self":[{"href":"https:\/\/c-mng.cwh.hokudai.ac.jp\/stl.eng\/Root\/wp-json\/wp\/v2\/pages\/2721"}],"collection":[{"href":"https:\/\/c-mng.cwh.hokudai.ac.jp\/stl.eng\/Root\/wp-json\/wp\/v2\/pages"}],"about":[{"href":"https:\/\/c-mng.cwh.hokudai.ac.jp\/stl.eng\/Root\/wp-json\/wp\/v2\/types\/page"}],"author":[{"embeddable":true,"href":"https:\/\/c-mng.cwh.hokudai.ac.jp\/stl.eng\/Root\/wp-json\/wp\/v2\/users\/2"}],"replies":[{"embeddable":true,"href":"https:\/\/c-mng.cwh.hokudai.ac.jp\/stl.eng\/Root\/wp-json\/wp\/v2\/comments?post=2721"}],"version-history":[{"count":7,"href":"https:\/\/c-mng.cwh.hokudai.ac.jp\/stl.eng\/Root\/wp-json\/wp\/v2\/pages\/2721\/revisions"}],"predecessor-version":[{"id":3181,"href":"https:\/\/c-mng.cwh.hokudai.ac.jp\/stl.eng\/Root\/wp-json\/wp\/v2\/pages\/2721\/revisions\/3181"}],"up":[{"embeddable":true,"href":"https:\/\/c-mng.cwh.hokudai.ac.jp\/stl.eng\/Root\/wp-json\/wp\/v2\/pages\/2646"}],"wp:attachment":[{"href":"https:\/\/c-mng.cwh.hokudai.ac.jp\/stl.eng\/Root\/wp-json\/wp\/v2\/media?parent=2721"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}
\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
\nFlow field around capsule with thin and large aeroshell (Density distribution).<\/p>\n
\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\n