Abstract

Two-point hot-wire measurements were conducted to assess the scaling of coherent structures in turbulent round jets. A scale-dependent coherence analysis was applied to datasets consisting of two-point synchronized axial velocity measurements with varying radial separations between the hot-wire positions while the reference hot-wire was fixed at the centreline and two off centreline positions in different datasets. Measurements were carried out at ReD=10000, 20000, and 50000 and a range of axial locations (3 ≤ x/D ≤ 25). The scale-dependent coherence analysis reveals a hierarchical structure of eddies over the axial range 15 ≤ x/D ≤ 25 for λx/y0.5 < 3, where λx is the axial wavelength and y0.5 is the jet half width. While these eddy structures are not geometrically self-similar at the centreline, away from the centreline they approach self-similarity status. In the jet shear-layer where the eddy structures are self-similar, a stochastic aspect ratio of ▪ ≈ 3.4 was found at ReD=10000. The aspect ratio increases to ▪ ≈ 3.9 at ReD=20000, and ▪ ≈ 4.7 at ReD=50000. These values are significantly smaller than the aspect ratio of ▪ =14 observed in turbulent boundary layers. The eddy structure aspect ratio is not affected by the axial distance from the nozzle (within x/D=15−25) or shear layer manipulation by control rings. However, the stochastic radial span of the largest eddies was found to change due to shear layer manipulation and change in the axial location.

Full Text
Paper version not known

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call

Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.