Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Satoru Takasaki"'
Autor:
Yoshiaki Wakumoto, Takashi Sakurai, Akimasa Someya, Yutaka Isobe, Satoru Takasaki, Katsunobu Okajima, Yuichi Tomiki, Kazuo Kempe, Yoshiaki Ito, Toshiaki Shimizu, Tomonosuke Someya, Takashi Dambara, Miyoko Tsukisawa, Hajime Arai, Takashi Murayama, Takeshi Nara, Masako Nishizuka, Tomoiku Takaku, Takanori Uka, Eiki Kominami, Tsutomu Suzuki, Etsuko Komiyama, Masataka Sumiyoshi, Yoshiyuki Ohtomo, Akira Murakami, Tetsuo Watanabe, Isao Nagaoka, Yusuke Suzuki
Publikováno v:
Juntendo Medical Journal. 58:248-255
Publikováno v:
TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B. 61:2798-2801
Publikováno v:
JSME International Journal Series B. 37:237-241
Chaotic mixing in two-dimensional square cavity flows with a time-periodic lid velocity was numerically simulated. To quantify the mixing in the cavity, the pseudo-Lyapunov exponent λ was measured. We selected the Reynolds number (Re) and amplitude
Publikováno v:
TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B. 60:1993-1998
A stochastic model which is used for simulating the time evolution of material line stretching in homogeneous turbulence is developed. Although the present model is similar to the Lagrangian random flight model, turbulent velocity is calculated for t
Publikováno v:
TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B. 57:2905-2908
Steady and 2D-driven cavity flows were numerically simulated using the finite difference method. Pseudo-Liapunov exponents were obtained by measuring distances between particles initially located nearby. In the case where the moving lid was oscillate
Inlet unstart influence on aerodynamic characteristics of next generation supersonic transport (SST)
Publikováno v:
AIAA and SAE, 1998 World Aviation Conference.
The impact of inlet unstart phenomena on supersonic transport (SST) was investigated by wind tunnel testing. Inlet unstart condition was simulated by controlling the captured mass flow by the inlet. Unsteady pressures on the lower surface of wing and
Akademický článek
Tento výsledek nelze pro nepřihlášené uživatele zobrazit.
K zobrazení výsledku je třeba se přihlásit.
K zobrazení výsledku je třeba se přihlásit.