Journal ArticleDOI
Transverse Injection Through Diamond and Circular Ports into a Mach 5.0 Freestream
TLDR
In this article, the authors compared the Reynolds-averaged Navier-Stokes and detached-eddy simulation models to obtain a detailed comparison of the secondary structures of the diamond-injector flowfield.Abstract:
Sonic transverse gaseous injection into a Mach 5.0 freestream flow was numerically simulated using two-equation and detached-eddy turbulence models. Circular- and diamond-shaped injectors were investigated in this study. The numerical simulations were compared with available experimental results and it was determined that both the Reynolds-averaged Navier-Stokes and detached-eddy simulation models captured the secondary flow structure. A detailed comparison of the secondary structures was performed for both injectors. Two new vortex structures of practical importance were observed in the diamond-injector flowfield. First, a leading-edge mixing mechanism was identified. Second, a trapped lateral counter-rotating vortex pair was produced. These new structures were observed in both Reynolds-averaged Navier-Stokes and detached-eddy simulation simulations. The detached-eddy simulations indicated that the large-scale structures observed in the plume/wake region of the flowfield were more organized in the diamond-injector test case. To better understand the secondary flow advection mechanism, the magnitudes of the terms in the compressible vorticity transport equation were compared. The diamond-injector structured-grid Reynolds-averaged Navier-Stokes solution was used as a baseline for this study. The inviscid compressibility, vortex-stretching, and baroclinic-torque terms were dominant. Downstream of the barrel-shock region, the baroclinic term was found to diminish when compared with the other inviscid terms. Planar-averaged results for the transport quantities confirmed this behavior. Vortex stretching was found to persist the longest.read more
Citations
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Journal ArticleDOI
Transverse jet in supersonic crossflows
TL;DR: In this article, the transverse jet in supersonic crossflows has been summarized systematically from four aspects, namely single injection, multiport injection, interaction between jet and vortex generator, and interaction between the jet and shock wave.
Journal ArticleDOI
Design exploration of three-dimensional transverse jet in a supersonic crossflow based on data mining and multi-objective design optimization approaches
TL;DR: In this paper, the effect of the injector geometric configuration on the mixing efficiency of the transverse injection flow field has been investigated, and four different configurations have been considered in the current study, namely the square port, the diamond ports, the equilateral triangular port and the circular port.
Journal ArticleDOI
Numerical investigation of transverse jets through multiport injector arrays in supersonic crossflow
Adrian Pudsey,Russell Boyce +1 more
TL;DR: Pudsey et al. as discussed by the authors performed a three-dimensional numerical study of the effects of sonic gaseous hydrogen injection through multiple transverse injectors subjected to a supersonic crossflow.
Journal ArticleDOI
Progress in research on mixing techniques for transverse injection flow fields in supersonic crossflows
Wei Huang,Li Yan +1 more
TL;DR: In this article, the transverse injection flow field has an important impact on the flowpath design of scramjet engines and the mixing process between the fuel and the supersonic freestream.
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