Numerical simulation of the two-phase nozzle flows with phase change effects
碩士 === 淡江大學 === 航空太空工程學系碩士班 === 102 === The purpose is to simulate the shock-like cavitation phenomena in the nozzle flow. Numerical simulation is based on the Roe type flux splitting method. The original ROE solver is reformulated in the algebraic form. This reformulated method can enhance the effi...
| Main Authors: | , |
|---|---|
| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2014
|
| Online Access: | http://ndltd.ncl.edu.tw/handle/yfg5dd |