Abstract
Convergent-divergent (C-D) ducts operating in supersonic flow-regimes provoke choked flow conditions in the region of the narrowest cross-section.
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References
Munday, D., Gutmark, E., Liu, J., Kailasanath, K.: Flow structure and acoustics of supersonic jets from conical convergent-divergent nozzles. Phys. Fluids 23, 116102 (2011)
Semlitsch, B., Mihăescu, M., Fuchs, L., Gutmark, E.: Numerical investigation of fluidic control on supersonic jet of a gas turbine engine. In: Proceedings of 20th International Shock Interaction Symposium, pp. 161–164 (2012)
Acknowledgments
This work was supported by the Swedish National Infrastructure for Computing (SNIC 002-12-11) via PDC.
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Semlitsch, B., Mihăescu, M., Fuchs, L. (2015). Large Eddy Simulation of Fluidic Injection into a Supersonic Convergent-Divergent Duct. In: Fröhlich, J., Kuerten, H., Geurts, B., Armenio, V. (eds) Direct and Large-Eddy Simulation IX. ERCOFTAC Series, vol 20. Springer, Cham. https://doi.org/10.1007/978-3-319-14448-1_37
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DOI: https://doi.org/10.1007/978-3-319-14448-1_37
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