Zobrazeno 1 - 10
of 50
pro vyhledávání: '"Etsuo Morishita"'
Autor:
Etsuo Morishita
This paper presents the project and experiment-based fluid dynamics education in Meisei University, a private institution in Tokyo, Japan. We pay attention not only to the basic engineering courses but also to the practical aspect of engineering expe
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::296c37944c866c227adcce3c5daf9a9d
Autor:
Etsuo Morishita
Publikováno v:
WIT Transactions on Engineering Sciences.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::869ecb45a693647d206416bf9378c1cb
https://doi.org/10.2495/afm160151
https://doi.org/10.2495/afm160151
Autor:
Etsuo Morishita
Publikováno v:
Topical Problems of Fluid Mechanics 2016.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6ecd17be11b9cc7071931d7bb0639b69
https://doi.org/10.14311/tpfm.2016.019
https://doi.org/10.14311/tpfm.2016.019
Autor:
Etsuo Morishita
Publikováno v:
Journal of Irrigation and Drainage Engineering. 135:704-707
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2cbc5a25946353d4e5e1094d4fdcf47c
https://doi.org/10.1061/(asce)ir.1943-4774.0000137
https://doi.org/10.1061/(asce)ir.1943-4774.0000137
Publikováno v:
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 51:139-145
Flows over two circular cylinders in tandem, side-by-side, and staggered arrangements were analyzed using the overset grid method, which is capable of handling a variety of sizes and arrangements. The Reynolds number was 100 based on the cylinder dia
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fb46c8ab4e3e62bf97b9f9e1731444c9
https://doi.org/10.2322/tjsass.51.139
https://doi.org/10.2322/tjsass.51.139
Autor:
Daisuke Maeda, Etsuo Morishita
Publikováno v:
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 49:117-124
Numerical simulations of the flow around a periodically vibrating airfoil and the two-degree-of-freedom (TDOF) bending-torsion flutter characteristics were carried out. An unsteady, two-dimensional, incompressible Navier-Stokes flow solver was couple
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2d4fd9561ebd41c5389587676f46ed24
https://doi.org/10.2322/tjsass.49.117
https://doi.org/10.2322/tjsass.49.117
Autor:
Etsuo Morishita, Hiroyoshi Asano
Publikováno v:
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 48:21-27
The oscillation of a circular cylinder in a uniform flow is not only one of the basic subjects of fluid dynamics, but is also a very important problem in fluids engineering. In the present paper, the cross-flow and in-line vibrations of a two-dimensi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::698fe1f78b5639d196d7240522b5944f
https://doi.org/10.2322/tjsass.48.21
https://doi.org/10.2322/tjsass.48.21
Autor:
Jianbo Zhang, Etsuo Morishita
Publikováno v:
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 47:90-98
An efficient way to systematically reproduce inflow profiles across a compressible, turbulent boundary layer for the mean flow variables, as well as the turbulent quantities in one-equation and two-equation turbulence-models, from given external flow
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cff34f8e59b58531cab8a5e6bc7e8378
https://doi.org/10.2322/tjsass.47.90
https://doi.org/10.2322/tjsass.47.90
Autor:
Etsuo Morishita
Publikováno v:
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 47:153-157
The classical Schwartz-Christoffel transformation can be extended to airfoils by a modern computational approach, which otherwise would be limited to calculating potential flows around simple geometric shapes. A numerical method is proposed to determ
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e121576e295d2eb4e72eacec211b4e0b
https://doi.org/10.2322/tjsass.47.153
https://doi.org/10.2322/tjsass.47.153
Publikováno v:
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 46:113-120
Three types of devices were tested for their effects in reducing the strong adverse pressure gradient in a closed-type cavity with a depth of 8 mm and length-to-depth ratio of 15. The first type of control device consisted of embedding arrays of tube
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a76aa74bc85f232afaa7927f26c70f8d
https://doi.org/10.2322/tjsass.46.113
https://doi.org/10.2322/tjsass.46.113