{"id":3299,"date":"2025-02-12T18:04:35","date_gmt":"2025-02-12T09:04:35","guid":{"rendered":"https:\/\/c-mng.cwh.hokudai.ac.jp\/stl.eng\/Root\/?p=3299"},"modified":"2025-02-12T18:08:25","modified_gmt":"2025-02-12T09:08:25","slug":"news-20250212","status":"publish","type":"post","link":"https:\/\/c-mng.cwh.hokudai.ac.jp\/stl.eng\/Root\/news\/news-20250212.html","title":{"rendered":"\u4ee4\u548c\uff16\u5e74\u5ea6\u5352\u8ad6\u4fee\u8ad6\u767a\u8868\u8aac\u660e\u4f1a"},"content":{"rendered":"<p>2025\/2\/4, 6\u306b\u5352\u8ad6\u4fee\u8ad6\u8aac\u660e\u4f1a\u304c\u884c\u308f\u308c\u307e\u3057\u305f\u3002\u4eca\u5e74\u5ea6\u3082\u5bfe\u9762\uff08\uff0b\u30aa\u30f3\u30e9\u30a4\u30f3\uff09\u3067\u306e\u958b\u50ac\u3068\u306a\u308a\u307e\u3057\u305f\u3002\u5f53\u7814\u7a76\u5ba4\u304b\u3089\u306f\u4e0b\u8a18\u306e\uff16\u540d\u304c\u767a\u8868\u3092\u3057\u307e\u3057\u305f\u3002<\/p>\n<p>\u5352\u696d\u8ad6\u6587\u767a\u8868\u8aac\u660e\u4f1a<\/p>\n<ul>\n<li>\u5927\u5ca1 \u614e\u4e5f<br \/>\n\u30a8\u30a2\u30d5\u30a3\u30eb\u30e0\u306b\u3088\u308b\u518d\u7a81\u5165\u6642\u306e\u7a7a\u529b\u52a0\u71b1\u4f4e\u6e1b\u5316\u7814\u7a76<br \/>\nReduction of aerodynamic heating during reentry by air film<\/li>\n<li>\u7551 \u58ee\u592a<br \/>\n\u8d85\u97f3\u901f\u9818\u57df\u306b\u304a\u3051\u308b\u67d4\u8edf\u69cb\u9020\u30a8\u30a2\u30ed\u30b7\u30a7\u30eb\u306e\u6d41\u4f53\u69cb\u9020\u9023\u6210\u89e3\u6790<br \/>\nFluid-structure interaction analysis of inflatable aeroshell in supersonic region<\/li>\n<\/ul>\n<div class=\"page\" title=\"Page 4\">\n<div class=\"section\"><\/div>\n<\/div>\n<p>\u4fee\u58eb\u8ad6\u6587\u767a\u8868\u8aac\u660e\u4f1a<\/p>\n<ul style=\"list-style-type: disc;\">\n<li>\u9152\u4e95\u667a\u57fa<br \/>\n\u8d85\u5c0f\u578b\u885b\u661f\u306e\u5b9f\u6e2cGNSS\u30c7\u30fc\u30bf\u306b\u57fa\u3065\u304f\u30c7\u30fc\u30bf\u540c\u5316\u624b\u6cd5\u306b\u3088\u308b\u5730\u7403\u8d85\u4f4e\u8ecc\u9053\u306e\u5927\u6c17\u5bc6\u5ea6\u63a8\u5b9a<br \/>\nEstimation of atmospheric density in very low Earth orbit based on GNSS data measured by nanosatellite using data assimilation method<\/li>\n<li>\u85e4\u7530\u8000\u4ecb<br \/>\n\u6d41\u4f53\u69cb\u9020\u9023\u6210\u89e3\u6790\u306b\u3088\u308b\u67d4\u8edf\u69cb\u9020\u30a8\u30a2\u30ed\u30b7\u30a7\u30eb\u306e\u59ff\u52e2\u4e0d\u5b89\u5b9a\u7814\u7a76<br \/>\nAttitude instability study of a flexible aeroshell using fluid-structure interaction analysis<\/li>\n<li>\u5409\u96c4\u5fe0\u884c<br \/>\n\u91cd\u5fc3\u4f4d\u7f6e\u304c\u8584\u6bbb\u30a8\u30a2\u30ed\u30b7\u30a7\u30eb\u578b\u30ab\u30d7\u30bb\u30eb\u306e\u4f4e\u901f\u57df\u59ff\u52e2\u4e0d\u5b89\u5b9a\u6027\u306b\u4e0e\u3048\u308b\u5f71\u97ff<br \/>\nThe effect of center of gravity on attitude instability of reentry capsule with thin aeroshell at subsonic speed<\/li>\n<li>Mohamed Elbasyouny<br \/>\n\u30aa\u30fc\u30d7\u30f3\u30bd\u30fc\u30b9\u30bd\u30d5\u30c8\u30a6\u30a7\u30a2\u3092\u7528\u3044\u305f\u4f4e\u30a2\u30b9\u30da\u30af\u30c8\u6bd4\u8907\u5408\u6750\u6599\u30af\u30ed\u30c3\u30d7\u30c9\u30c7\u30eb\u30bf\u7ffc\u306e\u7a7a\u529b\u5f3e\u6027\u30d5\u30e9\u30c3\u30bf\u30fc\u7279\u6027\u304a\u3088\u3073\u69cb\u9020\u8a2d\u8a08\u6539\u5584\u306b\u95a2\u3059\u308b\u6570\u5024\u7684\u7814\u7a76<br \/>\nNumerical investigation of the aeroelastic flutter characteristics of a low-aspect-ratio, composite cropped Delta wing, along with structural design improvement using open-source software<\/li>\n<\/ul>\n","protected":false},"excerpt":{"rendered":"<p>2025\/2\/4, 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