Zobrazeno 1 - 10
of 28
pro vyhledávání: '"フラッタ解析"'
Autor:
Tsukada, Harumi, Miyaji, Koji
Publikováno v:
宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2003論文集 = JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2003. :208-213
Two-dimensional aeroelastic problems at supersonic/transonic speeds are numerically simulated. Simplified structural computations are coupled with CFD code using unstructured grids with moving boundary. In panel flutter analyses, elastic deformations
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::a1bfca4f56827cd31483c7127e19d9dd
http://id.nii.ac.jp/1696/00006632/
http://id.nii.ac.jp/1696/00006632/
Publikováno v:
生産研究. 9(6):283-284
application/pdf
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::dea928625fda0cda1cfde642c3b9e134
https://repository.dl.itc.u-tokyo.ac.jp/records/23749
https://repository.dl.itc.u-tokyo.ac.jp/records/23749
Autor:
Yamasaki, Nobuhiko, Nanba, Masanobu
Publikováno v:
航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 41:161-166
航空宇宙技術研究所 24-26 Jun. 1998 東京 日本
National Aerospace Laboratory 24-26 Jun. 1998 Tokyo Japan
振動する翼列の線形非定常空気力計算は、計算機資源をあまり使用しないことと、非線形で
National Aerospace Laboratory 24-26 Jun. 1998 Tokyo Japan
振動する翼列の線形非定常空気力計算は、計算機資源をあまり使用しないことと、非線形で
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::00087e7296bf1c4ddba227cf8e0a83a3
http://id.nii.ac.jp/1696/00037331/
http://id.nii.ac.jp/1696/00037331/
Autor:
Kanda, Atsushi, Ueda, Tetsuhiko
Publikováno v:
航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory. 1380:1-22
有翼宇宙往還機HOPE-Xの計画が進んでいる。HOPE-Xの打上げ形態の一つにH-2ロケットの先端に搭載される方式が考えられている。このときHOPE-Xの動特性にロケットまたはロケット結合部によ
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::11df7e6d9f36b928d8f32c41dc7fd45c
http://id.nii.ac.jp/1696/00040318/
http://id.nii.ac.jp/1696/00040318/
Aeroelastic control of composite plate wings based on the optimal placement of sensors and actuators
Autor:
Kameyama, Masaki
Publikováno v:
宇宙航空研究開発機構特別資料 = JAXA Special Publication: Proceedings of Lectures and Workshop International: Recent Advances in Multidisciplinary Technology and Modeling. :121-130
The present paper treats the flutter suppression of composite plate wings with segmented piezoelectric sensors and actuators. First, fundamental mechanism of flutter suppression based on the measurement and control of specific vibration modes is exam
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::e10996f1aa5c53ee9a9953922fd9b693
http://id.nii.ac.jp/1696/00005661/
http://id.nii.ac.jp/1696/00005661/
Autor:
Machida, Kentaro, Miyaji, Koji
Publikováno v:
宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2005論文集 = JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2005. :94-99
A 3D flutter of a sweptback wing is numerically investigated by coupling inviscid flow simulations with a bending-torsion beam structure model. The beam model of a 3D wing is a natural extension of a widely used 2D 2-degree-of-freedom structure model
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::63a3c540d7626207f86c0b15df5367f7
http://id.nii.ac.jp/1696/00006142/
http://id.nii.ac.jp/1696/00006142/
Publikováno v:
航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory. 1228:1-20
チップフィン形状翼のフラッタ特性を把握するために基礎的な風洞実験を行った。模型を2体作り非平面翼のフラッタ解析のための実験データを得た。1体は通常の平面翼であり、もう1体
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::749c09d803a00ac29bc4d221677c4cc0
http://id.nii.ac.jp/1696/00041206/
http://id.nii.ac.jp/1696/00041206/
Autor:
Yang, Guowei, Obayashi, Shigeru
Publikováno v:
航空宇宙技術研究所特別資料: 航空宇宙数値シミュレーション技術シンポジウム2001論文集 = Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2001. 53:291-296
Through the coupling of subiteration between aerodynamic and structural governing equations, a full implicit finite-volume aeroelastic solver has been developed for transonic flutter simulation. The subiteration algorithm of the Navier-Stokes fluid e
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::5ffb70d4a63e827c876802d27a62c087
http://id.nii.ac.jp/1696/00038080/
http://id.nii.ac.jp/1696/00038080/
Autor:
Kanda, Atsushi
Publikováno v:
航空宇宙技術研究所特別資料: 第64回・第65回風洞研究会議論文集 = Special Publication of National Aerospace Laboratory: Proceedings of the 64th and 65th Workshop on Wind Tunnel Research. 51:79-83
In a case that a reentry winged space vehicle with non-planar wings like tip-fin is attached atop of a launch rocket, lateral modes due to attachments between the vehicle and the rocket or/and elasticity of the rocket may effect to flutter characteri
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::ed04e5587ab3bd74cc75fef718f60827
http://id.nii.ac.jp/1696/00038009/
http://id.nii.ac.jp/1696/00038009/