LES of an Inclined Jet into a Supersonic Turbulent Crossflow
Abstract
This short article describes flow parameters, numerical method, and animations of the fluid dynamics video "LES of an Inclined Jet into a Supersonic Turbulent Crossflow" (this http URL [high-resolution] and this http URL [low-resolution] video). We performed large-eddy simulation with the sub-grid scale (LES-SGS) stretched-vortex model of momentum and scalar transport to study the gas-dynamics interactions of a helium inclined round jet into a supersonic (M = 3.6) turbulent (Re_θ = 13×10^3) air flow over a flat surface. The video shows the temporal development of Mach-number and magnitude of density-gradient in the mid-span plane, and isosurface of helium mass-fraction and λ_2 (vortical structures). The identified vortical structures are sheets, tilted tubes, and discontinuous rings. The vortical structures are shown to be well correlated in space and time with helium mass-fraction isosurface (Y_(He) = 0.25).
Additional Information
This work was supported by AFOSR Grants FA9550-04-1-0020 and FA9550-04-1-0389, and by Caltech funds. The authors would like to thank Dr. C. Pantano for support with the AMROC software, the Center of Advanced Computing Research (CACR) at Caltech for computing time.Attached Files
Submitted - 0910.3018.pdf
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Additional details
- Eprint ID
- 99307
- Resolver ID
- CaltechAUTHORS:20191016-143406258
- Air Force Office of Scientific Research (AFOSR)
- FA9550-04-1-0020
- Air Force Office of Scientific Research (AFOSR)
- FA9550-04-1-0389
- Caltech
- Created
-
2019-10-16Created from EPrint's datestamp field
- Updated
-
2023-06-02Created from EPrint's last_modified field
- Caltech groups
- GALCIT