抄録
A finite-difference method is developed to solve a flow with a phase change by direct integration of the Navier-Stokes equations and the heat conduction equation. In the calculation, a moving grid is generated so that it fits smoothly the liquid-solid interface and strict boundary conditions can be imposed on that interface. Using this method, a pipe flow with unsteady solidification along the pipe wall was studied numerically.
本文言語 | English |
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ホスト出版物のタイトル | AlAA 23rd Aerospace Sciences Meeting, 1985 |
出版社 | American Institute of Aeronautics and Astronautics Inc, AIAA |
出版ステータス | Published - 1985 |
外部発表 | はい |
イベント | AlAA 23rd Aerospace Sciences Meeting, 1985 - Reno, United States 継続期間: 1985 1月 14 → 1985 1月 17 |
Other
Other | AlAA 23rd Aerospace Sciences Meeting, 1985 |
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国/地域 | United States |
City | Reno |
Period | 85/1/14 → 85/1/17 |
ASJC Scopus subject areas
- 航空宇宙工学