Zobrazeno 1 - 10
of 50
pro vyhledávání: '"Natsuki TSUSHIMA"'
Publikováno v:
Aerospace, Vol 11, Iss 8, p 637 (2024)
Phononic crystals based on lattice structures provide important wave dispersion characteristics as band structures, showing excellent compatibility with additive manufacturing. Although the lattice structures have shown the potential for vibration su
Externí odkaz:
https://doaj.org/article/a8cab39dee6943499da2588a5aa2974d
Publikováno v:
Aerospace, Vol 10, Iss 8, p 723 (2023)
By deliberately designing microscopic internal mechanisms, architected materials can achieve a variety of material properties without changing constituent materials. Integration of the architected materials into a structure as substructures has a goo
Externí odkaz:
https://doaj.org/article/ee66417f991e4024bf61ceb518de924b
Publikováno v:
Nihon Kikai Gakkai ronbunshu, Vol 86, Iss 890, Pp 19-00452-19-00452 (2020)
Various high-performance structures are ready to fabricate with the advent of the technology for the additive manufacturing. This additive manufacturing technology has a potential to improve manufacturing costs and may help to achieve high-performanc
Externí odkaz:
https://doaj.org/article/26b0802ebd8c49ba969836045b596549
Publikováno v:
Aerospace, Vol 8, Iss 8, p 200 (2021)
Additive manufacturing (AM) technology has a potential to improve manufacturing costs and may help to achieve high-performance aerospace structures. One of the application candidates would be a wind tunnel wing model. A wing tunnel model requires sop
Externí odkaz:
https://doaj.org/article/c60a081e2e804d1b91af3b45095b70eb
Geometrically nonlinear electro-aeroelastic framework for morphing wing with piezoelectric actuators
Publikováno v:
Nihon Kikai Gakkai ronbunshu, Vol 85, Iss 878, Pp 18-00506-18-00506 (2019)
In this paper, a flexible morphing wing with piezoelectric materials for morphing actuation is studied. The objectives of this paper are 1) to develop an integrated geometrically nonlinear electro-aeroelastic framework, which allows evaluating perfor
Externí odkaz:
https://doaj.org/article/f521158730cd49ca9b607cbfd7f3426f
Publikováno v:
Journal of Aircraft. 60:120-129
In this paper, an efficient aeroelastic model for morphing structures with corrugated panels is proposed, combining different fidelities of aerodynamic models. A finite element method with an actuation model is used to analyze the structural deformat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a8f56177f9f8d9bdde0260738c9ee863
https://doi.org/10.2514/1.c036692
https://doi.org/10.2514/1.c036692
Publikováno v:
International Journal of Aeronautical and Space Sciences. 23:723-733
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ce2658b3bd451dc2cd40757dad66966e
https://doi.org/10.1007/s42405-022-00474-3
https://doi.org/10.1007/s42405-022-00474-3
Publikováno v:
AIAA SCITECH 2023 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7985a93913cc7abc62da31cf181b8fcc
https://doi.org/10.2514/6.2023-2407
https://doi.org/10.2514/6.2023-2407
Publikováno v:
AIAA SCITECH 2023 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a01e29bd3858fa00a4d231a9567d026d
https://doi.org/10.2514/6.2023-2575
https://doi.org/10.2514/6.2023-2575
Publikováno v:
AIAA AVIATION 2022 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d5bd3a5ffc4f4bc7fd23752360c37280
https://doi.org/10.2514/6.2022-3418
https://doi.org/10.2514/6.2022-3418