Zobrazeno 1 - 10
of 10
pro vyhledávání: '"SANBONGI, Shigeo"'
Autor:
Sanbongi, Shigeo, Hamaguchi, Yasumasa
Publikováno v:
航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory. 1286:1-12
宇宙往還機の機体構造用候補材料であるカーボン/ポリイミド耐熱複合材料(T-800H/PMR-15)の強度特性評価の一環として、室温および300度C環境におけるスティフナの圧縮座屈強度および最終
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::5e1650cff343dc875aeef555bf52b1d6
http://id.nii.ac.jp/1696/00039756/
http://id.nii.ac.jp/1696/00039756/
Autor:
Kakuta, Yoshiaki, Sanbongi, Shigeo, Shimokawa, Toshiyuki, Hamaguchi, Yasumasa, Yamamoto, Masataka, Mitsuma, Hidehiko
Publikováno v:
航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory. 1254:1-28
本研究の目的は、小型の無人有翼宇宙往還機HOPE(H-2 Orbiting Plane)の主構造用候補材料として選択したカーボン/ポリイミド(T800H/PMR-15)複合材料の単層材特性データの取得と積層材強度を評価
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::89e7d49831a6cce316ac8b82a5793438
http://id.nii.ac.jp/1696/00041224/
http://id.nii.ac.jp/1696/00041224/
Autor:
Shimokawa, Toshiyuki, Hamaguchi, Yasumasa, Kakuta, Yoshiaki, Sanbongi, Shigeo, Morino, Yoshiki, Yamamoto, Masataka
Publikováno v:
航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory. 1238:1-15
本研究の目的は、2種類のカーボン/ポリイミド、Celion 6K/PMR-15とT800H/PMR-15準等方積層複合材料について、引張機械的性質を統計的に評価することである。2種の材料それぞれ約30個の平滑試
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::121f0522453a77514791d673299d8be4
http://id.nii.ac.jp/1696/00041214/
http://id.nii.ac.jp/1696/00041214/
Autor:
Shimokawa, Toshiyuki, Katoh, Hisaya, Hamaguchi, Yasumasa, Sanbongi, Shigeo, Mizuno, Hiroshi, Nakamura, Hiroyuki, Asagumo, Ryoji, Tamura, Hirobumi
Publikováno v:
Journal of Composite Materials; 2002, Vol. 36 Issue 7, p885, 11p
Publikováno v:
International Shipbuilding Progress; May 1971, Vol. 18 Issue: 201 p198-214, 17p
Publikováno v:
航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-994. 994:12
A component mode synthesis technique based on experimentally determined modal parameters is presented in this paper. The test structure is a solar array type plate, which is divided into three parts, and four flexible connective parts. In the synthes
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::e7439b8139a377e5625d4fd78b3eaeee
http://id.nii.ac.jp/1696/00045247/
http://id.nii.ac.jp/1696/00045247/
Autor:
SANBONGI, Shigeo, TODA, Susumu
Publikováno v:
航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-759. 759:16
The buckling strength of currugated shear webs was investigated. A finite element program containing a curved strip element was used in the analysis. Effects of geometrical parameters such as ratio of web depth to pitch and ratio of amplitude tp pitc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::57f20f414afb719cfe11e069045a1b33
http://id.nii.ac.jp/1696/00045011/
http://id.nii.ac.jp/1696/00045011/
Autor:
SANBONGI, Shigeo
Publikováno v:
航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-624. 624:19
The Compressive strength of flat stiffened panels is analysed and compared with experimental results. The elastic-plastis and geometric nonlinear analysis by the finite element method is carried out for short-panels. An experiment on the monolithic s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::0b472e2ce58d528bf6bb3b0e408a520e
http://id.nii.ac.jp/1696/00044873/
http://id.nii.ac.jp/1696/00044873/
Autor:
TAKENAKA, Yukihiko, SAITO, KOICHI, FURUTA, Toshiyasu, KAWASHIMA, Tsuneo, SANBONGI, Shigeo, OGAWA, Koichi, KOSHIDE, Shin-ichi, ASADA, Hiroo, KUMAKURA, Ikuo, OOTAKE, Kunihiko
Publikováno v:
航空宇宙技術研究所資料 = Technical Memorandum of National Aerospace Laboratory TM-133. 133:21
資料番号: NALTM0133000
レポート番号: NAL TM-133
レポート番号: NAL TM-133
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::beaf0d1b26f57d2f4338f75dbb931a2e
http://id.nii.ac.jp/1696/00043711/
http://id.nii.ac.jp/1696/00043711/
Autor:
SANBONGI, Shigeo
Publikováno v:
航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-165. 165:12
資料番号: NALTR0165000
レポート番号: NAL TR-165
レポート番号: NAL TR-165
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::a7b04725f4e601b73d0216e450dded8d
http://id.nii.ac.jp/1696/00044401/
http://id.nii.ac.jp/1696/00044401/