Theoretical investigation of effects of local cooling of a nozzle divergent section for controlling condensation shock in a supersonic two-phase flow of steam

DOI10.1007/S11012-012-9634-2zbMath1293.76078OpenAlexW2014817249MaRDI QIDQ399818

A. R. Teymourtash, E. Amiri Rad, Mohammad Reza Mahpeykar

Publication date: 20 August 2014

Published in: Meccanica (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s11012-012-9634-2

zbMATH Keywords

two-phase flownozzlecondensation shockvolumetric coolingwet steam

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Liquid-gas two-phase flows, bubbly flows (76T10) Supersonic flows (76J20)

Related Items (1)

On the application of isogeometric finite volume method in numerical analysis of wet-steam flow through turbine cascades

Cites Work

• Unnamed Item
• Suppression of condensation shock in wet steam flow by injection of water droplets in different regions of a Laval nozzle
• A pressure based Eulerian--Eulerian multi-phase model for non-equilibrium condensation in transonic steam flow
• Reduction of thermodynamic losses in a supersonic nucleating steam nozzle by spraying water droplets
• Study into nucleation of steam during expansion through a nozzle

This page was built for publication: Theoretical investigation of effects of local cooling of a nozzle divergent section for controlling condensation shock in a supersonic two-phase flow of steam