Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Nobuhiro Sekino"'
Autor:
Marilyn P. Glick, Robert Wardle, Gilles Bernard Vigier, I-Shih Chang, Toru Shimada, Didier Boury, B. D'Andrea, Hiroto Habu, Nobuhiro Sekino, John Napior, Jean-Francois Guery, Eric Robert, Max Calabro, Robert L. Glick, Christian Perut
Publikováno v:
Acta Astronautica. 66:201-219
著者人数:15名
Accepted: 2009-05-26
資料番号: SA1000722000
Accepted: 2009-05-26
資料番号: SA1000722000
Publikováno v:
AIAA Journal. 45(6):1324-1332
Accepted: 2006-11-28
資料番号: SA1001705000
資料番号: SA1001705000
Autor:
Keisuke Sawada, Eiji Shima, Ulrich Anzer, Mario Livio, Takanori Ishii, Takuya Matsuda, Nobuhiro Sekino
Publikováno v:
Monthly Notices of the Royal Astronomical Society. 255:183-191
Numerical simulations of 2D and 3D accretion flows past a gravitating compact object from a uniform flow at a large distance upstream are performed by solving the Eulerian equations. It is found that 2D flows exhibit a flip-flop instability if the ce
Publikováno v:
44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Accepted: 2009-07-23
資料番号: SA1000838000
資料番号: SA1000838000
Publikováno v:
36th AIAA Fluid Dynamics Conference and Exhibit.
Three-dimensional, single-phase (equilibrium two-phase) flows inside a solid rocket motor at three burn-back grain configurations are studied by computational fluid dynamics (CFD) analyses of the Reynolds-averaged Navier-Stokes equations (RANS). The
Autor:
Takashi Nakajima, Naoki Tamura, Nobuhiro Sekino, Toru Shimada, Masahiro Kohno, Yoshifumi Inatani
Publikováno v:
34th Aerospace Sciences Meeting and Exhibit.
In the design of M-V launch vehicle, computational fluid dynamics (CFD) has been used frequently in order to obtain design data, prediction models, and flowfield images. Numbers of simulations have been carried out dealing with various kinds of exter
Autor:
Hiroshi Hasegawa, Nobuyuki Tsuboi, Toru Shimada, Kazushige Kato, Hiroya Asakawa, Mihoko Fukunaga, Yu Daimon, Nobuhiro Sekino, Yoshio Seike
Publikováno v:
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN. 8:Pa_29-Pa_37
資料番号: SA1001703000
Publikováno v:
Monthly Notices of the Royal Astronomical Society. 236:817-828
Des simulations numeriques d'un ecoulement adiabatique axisymetrique passant a proximite d'une sphere rigide sont realisees en utilisant les equations d'Euler. Les resultats montrent que l'ecoulement est tres instable si le corps central n'est pas ab
Publikováno v:
Theory of Accretion Disks ISBN: 9789401069588
Numerical simulations of two-dimensional adiabatic inviscid flow in an accretion disc in a binary system or a proto-planetary system are performed using a second-order accurate implicit Roe upwind scheme. A purpose of the work is to estimate quantita
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::29cab86f44a9b67d9105cc1f3d0d9b80
https://doi.org/10.1007/978-94-009-1037-9_35
https://doi.org/10.1007/978-94-009-1037-9_35