Non-equilibrium rarefied flows are encountered frequently in supersonic flight at high altitudes, vacuum technology and in microscale devices. Prediction of the onset of non-equilibrium is important for accurate numerical simulation of such flows. We formulate and apply the discrete version of Boltz
Numerical simulation on non-equilibrium spontaneous condensation in supersonic steam flow
β Scribed by Yong Yang; Shengqiang Shen
- Publisher
- Elsevier Science
- Year
- 2009
- Tongue
- English
- Weight
- 396 KB
- Volume
- 36
- Category
- Article
- ISSN
- 0735-1933
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β¦ Synopsis
It is well known that the release of the latent heat by the homogenously nucleating steam flow can have a strong effect on the flow dynamics when the flow is transonic or supersonic with shock waves present. This paper describes a conservative two-dimensional compressible numerical model for supersonic nonequilibrium spontaneous condensing steam flow based on the classical nucleation theory and the Virial style equation of state. Quantitative validation of the numerical model was accomplished and the results showed a good agreement between numerical simulation and the experimental data. On the basis of the comparison of the proposed simulation and the dry isentropic expansion solution, the physical description of the condensation shock in Laval nozzles is concluded. And the effect of the condensation shock on the nucleation process itself and the resulting droplet size distribution was revealed.
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