Zobrazeno 1 - 10
of 27
pro vyhledávání: '"Keiichi ISHIKO"'
Publikováno v:
Journal of Fluid Science and Technology, Vol 12, Iss 3, Pp JFST0025-JFST0025 (2017)
A decomposition method of a given two-dimensional incompressible flow field into a dipole sequence is developed. Necessary condition for dipole sequence is revealed using a wavelet transform of di-vorticity of the given flow. Subsequently, a practica
Externí odkaz:
https://doaj.org/article/9492b17cc24741ed99f8796010b5acc5
Publikováno v:
Energies, Vol 4, Iss 10, Pp 1779-1839 (2011)
Hybrid Propulsion is an attractive alternative to conventional liquid and solid rocket motors. This is an active area of research and technological developments. Potential wide application of Hybrid Engines opens the possibility for safer and more fl
Externí odkaz:
https://doaj.org/article/0a0d7cd60d944c54ae1eb3911e4d02ac
Publikováno v:
AIAA Journal. 60:6557-6565
This study numerically investigated the characteristics of unsteady aerodynamic forces around a pitching airfoil in the transonic flow regime. The unsteady Reynolds-averaged compressible Navier–Stokes (URANS) equations were solved using a Spalart
Publikováno v:
The Proceedings of Conference of Hokkaido Branch. :41-42
Autor:
Yuya Shimada, Keiichi Ishiko
Publikováno v:
The Proceedings of Conference of Hokkaido Branch. :43-44
Autor:
Keiichi Ishiko, Tomonori Taniguchi
Publikováno v:
The Proceedings of Conference of Hokkaido Branch. :39-40
Publikováno v:
The Proceedings of Conference of Hokkaido Branch. :1322
Publikováno v:
55th AIAA Aerospace Sciences Meeting.
Autor:
Yuichi Matsuo, Akira Yoshizawa, Yoshiaki Nakamura, Yusuke Nishiyama, Keiichi Ishiko, Atsushi Hashimoto, Koichi Mori
Publikováno v:
Journal of Aircraft. 51:584-595
To predict the flowfield of three-dimensional wall jets, an extended nonlinear constitutive relation is incorporated into the Spalart–Allmaras turbulence model. A modification of the model is made to improve the predictability of free jets. The FaS
Publikováno v:
Scopus-Elsevier
Predicting transonic buffet over an aircraft is one of the challenging problems for current CFD community because the phenomenon is complex and unsteady. JAXA started to develop RANS/LES hybrid approaches to tackle unsteady flow problems including tr