| タイトル | Multiphase Modeling of Water Injection on Flame Deflector |
| 本文（外部サイト） | http://hdl.handle.net/2060/20130014503 |
| 著者（英） | Vu, Bruce T.; Peroomian, Oshin; Akdag, Vedat; Bachchan, Nili |
| 著者所属（英） | NASA Kennedy Space Center |
| 発行日 | 2013-06-24 |
| 言語 | eng |
| 内容記述 | This paper describes the use of an Eulerian Dispersed Phase (EDP) model to simulate the water injected from the flame deflector and its interaction with supersonic rocket exhaust from a proposed Space Launch System (SLS) vehicle. The Eulerian formulation, as part of the multi-phase framework, is described. The simulations show that water cooling is only effective over the region under the liquid engines. Likewise, the water injection provides only minor effects over the surface area under the solid engines. |
| NASA分類 | Spacecraft Propulsion and Power |
| レポートNO | KSC-2013-161 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
