Cooling Effect of Water Injection on a High-Temperature Supersonic Jet

The high temperature and high pressure supersonic jet is one of the key problems in the design of solid rocket motors. To reduce the jet temperature and noise, cooling water is typically injected into the exhaust plume. Numerical simulations for the gas-liquid multiphase flow field with mixture mult...

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Bibliografski detalji
Glavni autori: Jing Li, Yi Jiang, Shaozhen Yu, Fan Zhou
Format: Članak
Jezik:English
Izdano: MDPI AG 2015-11-01
Serija:Energies
Teme:
Online pristup:http://www.mdpi.com/1996-1073/8/11/12363