Summary
Computational simulation and study of shock/vortex interaction and vortex-breakdown modes are considered for bound (internal) and unbound (external) flow domains. The problem is formulated using the unsteady, compressible, full Navier-Stokes (NS) equations which are solved using an implicit, flux-difference splitting, finite-volume scheme. For the bound flow domain, a supersonic swirling flow is considered in a configured circular duct and the problem is solved for quasi-axisymmetric and three-dimensional flows. For the unbound domain, a supersonic swirling flow issued from a nozzle into a uniform supersonic flow of lower Mach number is considered for quasi-axisymmetric and three-dimensional flows. The results show several modes of breakdown; e.g., no-breakdown, transient single-bubble breakdown, transient multi-bubble breakdown, periodic multi-bubble multi-frequency breakdown and helical breakdown.
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References
Delery, J.; Horowitz, E.; Leuchter, O.; Solignac, J. L.: Fundamental Studies of Vortex Flows. La Recherche Aérospatiale, No. 1984–2, 1984, pp. 1–24.
Metwally, O.; Settles, G.; Horstman, C.: An Experimentally Study of Shock WaveNortex Interaction. AIAA 89–0082, January 1989.
Cutler, A. D.; Levey, B. S.: Vortex Breakdown in a Supersonic Jet. AIAA 91–1815, June 1991.
Rhode, D. L.; Lilley, D. G.; McLaughlin, D. K.: On the Prediction of Swirling Flowfields Found in Axisymmetric Combustor Geometries. Transactions of ASME Vol. 104, September 1982, pp. 378–384.
Altegeld, H.; Jones, W. P.; Wilhelmi: Velocity Measurements in a Confined Swirl Driven Recirculating Flow. Experiments in Fluids, Springer Verlag, Vol. 1, 1983, pp. 73–78.
Liu, C. H.; Krause, E.; Menne, S.: Admissible Upstream Conditions for Slender Compressible Vortices. AIAA 86–1093, 1986.
Copening, G.; Anderson, J.: Numerical Solutions to Three-Dimensional Shock/Vortex Interaction at Hypersonic Speeds. AIAA 89–0674, January 1989.
Kandil, O. A.; Kandil, I-1. A.: Computation of Compressible Quasi-Axisymmetric Slender Vortex Flow and Breakdown. IMACS 1st International Conference on Computational Physics, University of Colorado, Boulder, June 1990, pp. 46–51. Also in Computer Physics Communications Vol. 65, North-Holland, March 1991, pp. 164–172.
Meadows, K.; Kumar, A.; Hussaini, M.: A Computational Study on the Interaction Between a Vortex and a Shock Wave. AIAA 89–1043, April 1989:
Kandil, O. A.; Kandil, H. A.; Liu, C. H.: Computation of Steady and Unsteady Compressible Quasi-Axisymmetric Vortex Flow and Breakdown. AIAA 91–0752, January 1991.
Kandil, O. A.; Kandil, H. A.; Liu, C. H.: Supersonic Quasi-Axisymmetric Vortex Breakdown. AIAA 91–3311-CP, September 1991, pp. 851–863.
Kandil, O. A.; Kandil, H. A.; Liu, C. H.: Critical Effects of Downstream Boundary Conditions on Vortex Breakdown. AIAA 92–2601-CP, June 1992.
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© 1993 Springer-Verlag Berlin Heidelberg
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Kandil, O.A., Kandil, H.A., Liu, C.H. (1993). Shock/Vortex Interaction and Vortex-Breakdown Modes. In: Kawamura, R., Aihara, Y. (eds) Fluid Dynamics of High Angle of Attack. International Union of Theoretical and Applied Mechanics. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-52460-8_13
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DOI: https://doi.org/10.1007/978-3-642-52460-8_13
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