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On the Flow Physics of a Low Momentum Flux Ratio Jet in a Supersonic Turbulence Crossflow

You, Yancheng and Lüdeke, Heinrich and Hannemann, Klaus (2012) On the Flow Physics of a Low Momentum Flux Ratio Jet in a Supersonic Turbulence Crossflow. Europhysics Letters, Vol. 97 (2). IOPScience. DOI: 10.1209/0295-5075/97/24001. ISSN 0295-5075 .

Full text not available from this repository.

Official URL: http://iopscience.iop.org/0295-5075/97/2/24001

Abstract

Detached Eddy Simulations (DES) study of the low momentum flux ratio jet, J = (ρu2 )jet /(ρu2 )∞ = 0.35, in the HyShot II scramjet system is carried out. The flow structure near the injector, shock pattern in the symmetry plane as well as the instantaneous coherent structures are presented and explained in the paper. Different from most previous studies, over-expanded and under-expanded flow states occur simultaneously at the exit of the current jet porthole. The shock system near the injector is therefore a combination of detached normal shock and a small three-dimensional barrel shock ended with a Mach disk. Further insight into the flow physics is conducted by visualizing instantaneous coherent structures. The formation of Ω shaped vortex, which was observed in experiments previously, but never well-studied numerically, is discussed in detail. A new understanding of the key flow physics and mixing patterns in the low-momentum flux-ratio jet in supersonic crossflow is finally schematically provided.

Document Type:Article
Title:On the Flow Physics of a Low Momentum Flux Ratio Jet in a Supersonic Turbulence Crossflow
Authors:
AuthorsInstitution or Email of Authors
You, Yanchengyancheng.you@dlr.de
Lüdeke, Heinrichheinrich.luedeke@dlr.de
Hannemann, Klausklaus.hannemann@dlr.de
Date:2012
Journal or Publication Title:Europhysics Letters
Refereed publication:Yes
In Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:Vol. 97
DOI:10.1209/0295-5075/97/24001
Publisher:IOPScience
Series Name:EPL(Europhysics Letters)
ISSN:0295-5075
Status:Published
Keywords:Turbulent jets, Mixing, Hydrogen injection, Detached Eddy Simulation, Scramjet
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - EU Projekte Raumtransport
Location: Braunschweig , Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Yancheng You
Deposited On:30 Nov 2011 11:38
Last Modified:26 Mar 2013 13:34

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