In this work, we try to find the best setting of Computational Fluid Dynamic solver available for the problems in the field of supersonic internal flows. We used the supersonic air-toair ejector to represent the typical problem in focus. There are multiple oblique shock waves, shear layers, boundary layers and normal shock interacting in the supersonic ejector making this device typical in field of supersonic inner flows. Modeling of shocks in general is demanding on the physical model of fluid, because ordinary conservation equation does not conform to real conditions in the near-shock region as found in many works. From these reasons, we decided to take special care about solver setting in this article by means of experimental approach of color Schlieren pictures and pneumatic measurement. Fast pressure transducers were used to measure unsteady static pressure in regimes with normal shock in mixing chamber. Physical behavior of ejector in several regimes is discussed. Best choice of eddy-viscosity setting is discussed on the theoretical base. The final verification of the k-ω SST is done on the base of comparison between experiment and numerical results., {"references":["Breitkopf, P. and Coelho, R. F. Multidisciplinary design optimization in\ncomputational mechanics: Wiley-ISTE, 2010. ISBN-10 1848211384.","Hynek, J. Genetic algorithms and genetic programing (in Czech).\nPrague : Grada Publishing ,a. s., 2008. ISBN 978-80-247-2695-3.","Dvoř├ík, V. and Kol├íř, J. Shape optimization of supersonic ejectors with\nseveral primary nozzles. Lisboa, Portugal : In the 2nd International\nConference on Engineering Optimization, 6.-9. september 2010. ISBN\n978-989-96264-3-0.","Dvoř├ík, V. Shape optimization of supersonic ejector for supersonic\nwind tunnel. s.l. : In.: Applied and Computational Mechanics, 2010. pp.\n15-24. ISSN 1802-680X.","Kol├íř, J. and ┼áafař├¡k, P. Interaction of oblique shock wave with shear\nlayer. Plzeň : In Proceedings of the International Conference XXVII:\nMeeting of Departments of Fluid Mechanics and Thermomechanics,\n2008. pp. 163-170. ISBN 978-80-7043-666-0.","Moeckel, W. E. Interaction of oblique shock waves with regions of\nvariable pressure, entropy and energy. Washington : NACA, 1952. TN\n2725.","Shapiro, A. H. The dynamics and thermodynamics of compressible\nfluid flow. New York : The Ronald Press Company, 1953. ISBN\n0826080758.\n8] Versteeg, H. K. and Malalasekera, W. An Introduction to\nComputational fluid dynamics, The Finite Volume Method: Pearson\nEducation Limited 2007, ISBN 978-0-13-127498-3.","Wilcox, D. Reassessment of the scale determining equation for\nadvanced turbulent models. 1988. AIAA J. 26 (11),1299-1310.\n[10] Menter, F. R. Two-equations Eddy-viscosity turbulence models for\nengineering applications. 1994. AIAA J. 32(8), 1598-1605.\n[11] Inc., Fluent. Fluent user documentation. Lebanon : s.n., 2006.\nfrom the biography."]}