Presentation of Flow Case
The present report summarizes the activities that have been performed for flow case 3.1 (TUD impinging-shock case) within the context of the European Commission 6th Framework Programme ‘UFAST – Unsteady Effects in Shock Wave Induced Separation’, contract number 012226 (AST4-CT- 2005-012226). The experimental measurements for the case study have been performed at the High Speed Laboratory of the Delft University of Technology department of Aerospace Engineering (partner 7: TUD) The flow case consists in the reflection of an oblique shock from a planar surface in the low supersonic regime. Data have been acquired for a free-stream ofMach 1.7 with an incident shock wave corresponding to a flow deflection of 6o. The peculiar feature of the experiment is the very large Reynolds number (Re θ ≈ 50000), in view of the substantial boundary layer thickness (δ 99 = 17mm) and high stagnation pressure (230 kPa) upstream of the interaction zone. Particle Image Velocimetry (PIV) has been applied as major diagnostic tool for the investigation of the interaction, both in the standard form (planar two-components and stereo) and in more advanced configurations (notably, Dual-plane and Tomographic PIV).
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References
Delery, J., Marvin, J.G.: Shock-wave boundary layer interactions. AGARDograph 280 (1986)
Ducros, F., Ferrand, V., Nicoud, F., Darracq, D., Gacherieu, C., Poinsot, T.: Large-eddy simulation of the shock/turbulence interaction. J. Comput. Phys. 152, 517–549 (1999)
Fares, E., Schröder, W.: A general one-equation turbulence model for free shear and wall-bounded flows. Flow, Turbulence and Combustion 73, 187–215 (2004)
Ganapathisubramani, B., Clemens, N.T., Dolling, D.S.: Effects of upstream boundary layer on the unsteadiness of shock-induced separation. J. Fluid Mech. 585, 369–394 (2007)
Hanjalic, K.: Will RANS survive LES? a view of perspectives. J. Fluids Eng. 127, 831–839 (2005)
Inagaki, M., Kondoh, T., Nagano, Y.: A mixed-time-scale sgs model with fixed model-parameters for practical LES. J. Fluids Eng. 127(1), 1–13 (2005)
Klein, M., Sadiki, A., Janicka, J.: A digital filter based generation of inflow data for spatially developing direct numerical or large eddy simulations. J. Comput. Phys. 186, 652–665 (2003)
Li, Q., Coleman, G.N.: DNS of an oblique shock wave impinging upon a turbulent boundary layer. In: Geurts, Friedrich, Metais (eds.) Direct and Large-Eddy Simulations. Ercoftac Series, pp. 387–396. Kluwer, Dordrecht (2003)
Pirozzoli, S., Grasso, F.: Direct Numerical Simulation of isotropic compressible turbulence: Influence of compressibility on dynamics and structures. Phys. Fluids 16(12), 4386–4407 (2004)
Pirozzoli, S., Grasso, F.: Direct Numerical Simulation of impinging shock-wave/turbulent boundary layer interaction at M= 2.25. Phys. Fluids 18(6), 1–17 (2006)
Sagaut, P.: Large-Eddy Simulation for Incompressible Flows: An Introduction to Large-Eddy Simulations. Springer, Heidelberg (2001)
Sandham, N.D., Li, Q., Yee, H.C.: Entropy slitting for high-order numerical simulation of compressible turbulence. J. Comput. Phys. 178, 307–322 (2002)
Sandham, N.D., Yao, Y.F., Lawal, A.A.: Large-Eddy Simulation of transonic turbulent flow over a bump. Int. J. Heat and Fluid Flow 24(4), 584–595 (2003)
Smits, A.J., Dussauge, J.P.: Turbulent Shear Layers in Supersonic Flow. American Institute of Physics, New York (2006)
Souverein, L., Dupont, P., Debiéve, J., Dussauge, J.P., van Oudheusden, B.W., Scarano, F.: Unsteadiness characterization in a shock wave turbulent boundary layer interaction through dual-PIV. AIAA Paper 2008-4169 (2008a)
Souverein, L.J., van Oudheusden, B.W., Scarano, F., Dupont, P.: Unsteadiness characterization in a shock wave turbulent boundary layer interaction through dual-PIV. AIAA Paper 2008-4169 (2008b)
Souverein, L.J., van Oudheusden, B.W., Scarano, F., Dupont, P.: Application of a dual-plane particle image velocimetry (dual-PIV) technique for the unsteadiness characterization of a shock wave turbulent boundary layer interaction. Meas. Sci. Technol. 20, 074003.1–074003.16 (2009)
Spalart, P., Allmaras, S.: A one-equation turbulence model for aerodynamic flows. La Recherche Aérospatiale 1, 5–21 (1994)
Thompson, K.W.: Time dependent boundary conditions for hyperbolic systems. J. Comput. Phys. 68, 1–24 (1987)
Touber, E., Sandham, N.D.: Large-Eddy Simulation of low-frequency unsteadiness in a turbulent shock-induced separation bubble. Theoretical and Computational Fluid Dynamics (2009) (accepted for publication)
van Oudheusden, B.W.: Principles and application of velocimetry-based planar pressure imaging in compressible flows with shocks. Exp. Fluids 45, 657–674 (2008)
Wilcox, D.: Reassessment of the scale-determining equation for advanced turbulence models. AIAA J. 11, 1299–1310 (1988)
Wilcox, D.: Turbulence modeling for CFD. DCW Industries (1998)
Yee, H.C., Sandham, N.D., Djomehri, M.J.: Low-dissipative high-order shock-capturing methods using characteristic-based filters. J. Comput. Phys. 150, 199–238 (1999)
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Doerffer, P., Hirsch, C., Dussauge, JP., Babinsky, H., Barakos, G.N. (2010). Oblique Shock Reflection at M = 1.7 (Sergio Pirozzoli). In: Unsteady Effects of Shock Wave Induced Separation. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 114. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-03004-8_8
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