The flow in supersonic annular jets has been investigated experimentally. Schemes for shock interaction during reconstruction from an open to a closed base region are determined. The fundamental parameters characterizing the structure of the separation flow are extracted.
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Shvets, A.I. Supersonic annular jet. J Appl Mech Tech Phys 16, 201–208 (1975). https://doi.org/10.1007/BF00858914
- Mathematical Modeling
- Mechanical Engineer
- Industrial Mathematic
- Base Region
- Separation Flow