Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Junya Aono"'
Autor:
Junya AONO, Keiichi KITAMURA
Publikováno v:
Journal of Fluid Science and Technology, Vol 18, Iss 1, Pp JFST0016-JFST0016 (2023)
Multiphase flows arise in various fields that involve complicated phenomena. Studies have shown that COVID-19 can occur via air microdroplets, and breathing jets with microdroplets turn into turbulent cloud or puffs in cases of coughing and sneezing
Externí odkaz:
https://doaj.org/article/9e93d51cdbe24c379719e8ef5535c3a4
Autor:
Susumu Hasegawa, Kan Kobayashi, Sadatake Tomioka, Taro Shimizu, Masatoshi Kodera, Junya Aono, Toshihiko Munakata, Masahiro Takahashi
Publikováno v:
Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan. 19(3):415-423
形態: カラー図版あり
Physical characteristics: Original contains color illustrations
Accepted: 2020-06-15
資料番号: PA2110054000
Physical characteristics: Original contains color illustrations
Accepted: 2020-06-15
資料番号: PA2110054000
Autor:
Junya, Aono, Keiichi, Kitamura
Publikováno v:
Journal of Computational Physics. 462:111256
This paper proposes a novel method for the computation of compressible multiphase flows under the assumption of pressure equilibrium based on a 6-equation model and the AUSM (Advection Upstream Splitting Method) family. In this study, we introduce a
Autor:
Masahiro TAKAHASHI, Sadatake TOMIOKA, Masatoshi KODERA, Kan KOBAYASHI, Susumu HASEGAWA, Taro SHIMIZU, Junya AONO, Toshihiko MUNAKATA
Publikováno v:
Transactions of the Japan Society of Aeronautical & Space Sciences, Aerospace Technology Japan; 2021, Vol. 19 Issue 3, p415-423, 9p
Publikováno v:
Journal of Spacecraft and Rockets. 50:896-916
Accepted: 2012-08-13
資料番号: SA1004435000
資料番号: SA1004435000
Autor:
Junya Aono, Kazuto Kuzuu
Publikováno v:
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
The overset grid approach provides a very powerful means of handling complex geometries in computational fluid dynamics. This overset grid approach has many advantages for the moving boundary or the rudders problem. Therefore, an overset unstructured
Publikováno v:
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
Flight capability of a reusable sounding rocket during turnover was investigated by numerical analysis. In this study, we first carried out the numerical flow simulation to obtain aerodynamic characteristics in turnover maneuver, and then solved kine
Autor:
Keiichi Kitamura1,2,3,4, Satoshi Nonaka1,4,5, Kazuto Kuzuu1,4,6, Junya Aono7, Keiichiro Fujimoto4,8,9, Eiji Shima1,4,10
Publikováno v:
Journal of Spacecraft & Rockets. Jul/Aug2013, Vol. 50 Issue 4, p896-916. 21p.