Abstract
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.
| Original language | English |
|---|---|
| Title of host publication | AlAA 23rd Aerospace Sciences Meeting, 1985 |
| Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
| Publication status | Published - 1985 |
| Externally published | Yes |
| Event | AlAA 23rd Aerospace Sciences Meeting, 1985 - Reno, United States Duration: 1985 Jan 14 → 1985 Jan 17 |
Other
| Other | AlAA 23rd Aerospace Sciences Meeting, 1985 |
|---|---|
| Country/Territory | United States |
| City | Reno |
| Period | 85/1/14 → 85/1/17 |
ASJC Scopus subject areas
- Aerospace Engineering