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Abstract
In the present study, a computational fluid dynamics method has been applied to investigate the effects of initial degree of supersaturation at reservoir condition on under-expanded sonic jet structures, such as Mach disk location and diameter, barrel shock wave and jet boundary. The axisymmetric nozzle geometry investigated was a contoured converging nozzle with straight part. As a result, it was found that the characteristics of flow with occurrence of non-equilibrium condensation in the jet were different from those without condensation.
Journal
- 年次大会講演論文集 : JSME annual meeting [List of Volumes]
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年次大会講演論文集 : JSME annual meeting 2006(2), 113-114, 2006-09-15 [Table of Contents]
The Japan Society of Mechanical Engineers