Large Eddy Simulation of the Laminar-Turbulent Transition in the Flow Induced by Wall Injection
被引:5
作者:
Gazanion, B.
论文数: 0引用数: 0
h-index: 0
机构:
CNES, Direct Lanceurs, 52 Rue Jacques Hillairet, F-75612 Paris, France
Off Natl Etud & Rech Aerosp, F-31055 Toulouse 4, FranceCNES, Direct Lanceurs, 52 Rue Jacques Hillairet, F-75612 Paris, France
Gazanion, B.
[1
,2
]
Chedevergne, F.
论文数: 0引用数: 0
h-index: 0
机构:
Off Natl Etud & Rech Aerosp, F-31055 Toulouse 4, FranceCNES, Direct Lanceurs, 52 Rue Jacques Hillairet, F-75612 Paris, France
Chedevergne, F.
[2
]
Casalis, G.
论文数: 0引用数: 0
h-index: 0
机构:
Off Natl Etud & Rech Aerosp, F-31055 Toulouse 4, FranceCNES, Direct Lanceurs, 52 Rue Jacques Hillairet, F-75612 Paris, France
Casalis, G.
[2
]
机构:
[1] CNES, Direct Lanceurs, 52 Rue Jacques Hillairet, F-75612 Paris, France
[2] Off Natl Etud & Rech Aerosp, F-31055 Toulouse 4, France
来源:
IUTAM-ABCM SYMPOSIUM ON LAMINAR TURBULENT TRANSITION
|
2015年
/
14卷
关键词:
Large Eddy Simulation;
vortex shedding;
laminar-turbulent transition;
wall injection;
DIRECT NUMERICAL-SIMULATION;
STABILITY;
D O I:
10.1016/j.piutam.2015.03.072
中图分类号:
O3 [力学];
学科分类号:
08 ;
0801 ;
摘要:
Laminar-turbulent transition of an experimental configuration representative of the flow in Solid Rocket Motors is investigated using Large Eddy Simulation. The specific instability of this flow is reproduced and a turbulent region is recovered, using a spatial perturbation model built upon an analysis of the noise related to injection. The results show the axial natural growth of instabilities until the laminar-turbulent transition occurs near the end of the channel. Comparisons to measurements are made to validate the numerical procedure. (C) 2014 The Authors. Published by Elsevier B.V.