Zobrazeno 1 - 10
of 44
pro vyhledávání: '"Yoshiki Morino"'
Publikováno v:
Aerospace Science and Technology. 38:48-55
A transient inverse heat conduction analysis enables the identification of the unknown boundary heat flux from finite number of temperature data obtained, e.g., in the high temperature structural tests or in the actual operation. Since the prediction
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2288622f9c30c87061319415dc397f0c
http://id.nii.ac.jp/1696/00022588/
http://id.nii.ac.jp/1696/00022588/
Publikováno v:
Acta Astronautica. 94:318-327
The amount of space debris is ever increasing, and pollution of the space environment has become a serious problem that can no longer be ignored. Consequently, the active removal of large space debris from crowded economically useful orbits should be
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ef02329dcf74beab27569044e898f9e7
https://doi.org/10.1016/j.actaastro.2013.03.024
https://doi.org/10.1016/j.actaastro.2013.03.024
Autor:
Takashi Ishikawa, Yoichi Hayashi, Yoshiki Morino, Tomohiro Yokozeki, Takayuki Shimoda, Tetsuya Morimoto
Publikováno v:
Advanced Composite Materials. 13:81-88
Two liner-less CFRP concept tanks were prepared for internal pressurization tests at liquefied nitrogen (LN2) temperature. The tanks were designed in two patterns of eight-ply UD quasi-isotropic lay-up, in the shape as a cylinder of 600 mm in diamete
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::958a00c8d10b3c33902b3636f621d989
https://doi.org/10.1163/1568551041718062
https://doi.org/10.1163/1568551041718062
Publikováno v:
AIP Conference Proceedings.
Fiber Bragg Grating (FBG) sensors have widely been used to monitor temperature and strain distributions as a part of the structural health monitoring system. Since FBG has the sensitivity to the variations in both temperature and strain, a compensati
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::63fc137e7bae7b5fca5b23c2872878c7
https://doi.org/10.1063/1.4904642
https://doi.org/10.1063/1.4904642
Publikováno v:
Advanced Composite Materials. 10:339-347
It is essential to utilize carbon fiber reinforced plastics (CFRP) for main structural materials of cryogenic propellant tanks in order to realize the drastic weight reduction needed for efficient reusable space transportation systems. Recently devel
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1b75856be9bb0041ef00941d7de40afe
https://doi.org/10.1163/156855101753415364
https://doi.org/10.1163/156855101753415364
Autor:
Yoshiki Morino
Publikováno v:
Journal of the Japan Society for Aeronautical and Space Sciences. 46:471-475
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::146e9d54743241edc09afe5371089508
https://doi.org/10.2322/jjsass1969.46.471
https://doi.org/10.2322/jjsass1969.46.471
Publikováno v:
Journal of the Japan Society for Composite Materials. 24:169-175
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::24a7a4beef9a9c1471ad9bc1fbd9016a
https://doi.org/10.6089/jscm.24.169
https://doi.org/10.6089/jscm.24.169
Publikováno v:
AIP Conference Proceedings.
Thermal analysis is required in the design of the structure of atmospheric reentry vehicles, which are subjected to severe aerodynamic heating. However, prediction of aerodynamic heating is difficult owing to highly complex physical phenomena. Invers
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::af9ef10a609ad4c453b1dd09f11d7b95
https://doi.org/10.1063/1.4765536
https://doi.org/10.1063/1.4765536
Autor:
Yoshiki Morino
Publikováno v:
Journal of the Japan Welding Society. 62:617-622
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f043d4953e5eea7cbd5a6d90c2442fa4
https://doi.org/10.2207/qjjws1943.62.617
https://doi.org/10.2207/qjjws1943.62.617
Publikováno v:
Journal of Intelligent Material Systems and Structures. 3:697-718
Control/structure interaction problems are much concerned with the atti tude stability of space structures and the accuracies of on-board instruments as the sizes and flexibilities of structures increase. In this paper, an attempt to integrate colloc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e1f5640a482923f116d496bd75ad7bf1
https://doi.org/10.1177/1045389x9200300411
https://doi.org/10.1177/1045389x9200300411