Zobrazeno 1 - 10
of 73
pro vyhledávání: '"Tsutahara, Michihisa"'
Publikováno v:
In Computers and Mathematics with Applications 2010 59(7):2403-2410
Publikováno v:
In Computers and Mathematics with Applications 2010 59(7):2411-2420
Publikováno v:
In International Journal of Multiphase Flow 2008 34(9):852-864
Autor:
Tsutahara, Michihisa
Publikováno v:
数理解析研究所講究録. 1946:31-40
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::f5778eff56c0441b14023a2bcdf485ee
http://hdl.handle.net/2433/223882
http://hdl.handle.net/2433/223882
Publikováno v:
In European Journal of Mechanics / B Fluids 2001 20(2):167-186
Publikováno v:
In Computer Physics Communications 2000 129(1):131-137
Autor:
Michiwaki, Akira, Tsutahara, Michihisa, Mae, Kentaro, Mori, Masaharu, Aoyama, Takashi, Murakami, Keiichi
Publikováno v:
Memoirs of the Graduate Schools of Engineering and System Informatics Kobe University. 2:1-7
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::2a686ca78bdef7078454e47cce99239f
https://hdl.handle.net/20.500.14094/81002735
https://hdl.handle.net/20.500.14094/81002735
Publikováno v:
宇宙航空研究開発機構特別資料: 第39回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2007論文集 = JAXA Special Publication: Proceedings of 39th Fluid Dynamics Conference/Aerospace Numerical Simulation Symposium 2007. :39-44
Parallel blade-vortex interactions have been calculated using the finite difference lattice Boltzmann method of the compressible Euler model. The perturbed discrete Boltzmann equation based on a prescribed vortex method has been proposed in order to
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::3e7a911a11cbdd63fc68499af79148a0
http://id.nii.ac.jp/1696/00005607/
http://id.nii.ac.jp/1696/00005607/
Autor:
Hiraishi, Masayuki, Tsutahara, Michihisa, Tajiri, Shinsuke, Murakami, Keiichi, Aoyama, Takashi
Publikováno v:
宇宙航空研究開発機構特別資料: 第39回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2007論文集 = JAXA Special Publication: Proceedings of 39th Fluid Dynamics Conference/Aerospace Numerical Simulation Symposium 2007. :113-118
The acoustic noise generated by the jet of a rocket launching becomes a serious problem for an on-board satellite now. It has been known that we can reduce this noise by spraying water into the jet. But this mechanism is not clarified. In this report
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::d3fb3756b68defca1c343d44d83e4510
http://id.nii.ac.jp/1696/00005618/
http://id.nii.ac.jp/1696/00005618/
Publikováno v:
The Proceedings of Conference of Kansai Branch. :4-23
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8e5ee92993025c7e662234369374a931
https://doi.org/10.1299/jsmekansai.2005.80._4-23_
https://doi.org/10.1299/jsmekansai.2005.80._4-23_