Abstract
Results of numerical simulations of a supersonic flow in a channel with a rectangular cross section having a longitudinally ribbed bottom surface are reported. The channel contains a tapered inlet section, where the cowl lip generates a shock wave incident onto the bottom surface, and a posterior constant-area section. The present numerical simulations are performed for a viscous three-dimensional flow with the use of the Reynolds-averaged Navier-Stokes equations and k-ω SST turbulence model. The computations are performed for the free-stream Mach number M = 4.
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References
J. Seddon and E. Goldsmith, Intake aerodynamics, AIAA Education Ser., Reston, 1985.
D.M. van Wie, Scramjet intakes, in: Scramjet Propulsion, E.T. Curran and S.N.B. Murthy (Eds.), Progress in Astronautics and Aeronautics, 2000, Vol. 189, P. 447–511.
Yu.P. Gounko and I.I. Mazhul, Gas-dynamic design of a two-dimensional supersonic inlet with the increased flow rate factor, Thermophysics and Aeromechanics, 2012, Vol. 19, No. 4, P. 363–379.
F. Falempin, M.A. Goldfeld, Yu.V. Semenova, A.V. Starov, and K.Yu. Timofeev, Experimental study of different control methods for hypersonic air inlets, Thermophys. Aeromech., 2008, Vol. 15, No. 1, P. 1–9.
M.A. Goldfeld, Effect of flow velocity on inlet compression surfaces on the efficiency of boundary layer bleeding, Sib. Fiz. Zh., 2019, Vol. 14, No. 3, P. 15–25.
V.V. Zatoloka and G.A. Kisel, Swept surface boundary layer bleeding in a hypersonic convergent inlet, Fiz. Gazodinamika (Aerofiz. Issled. No. 6), ITAM SB RAS, Novosibirsk, 1976, P. 61–62.
Yu.P. Gounko, I.I. Mazhul, and A.M. Kharitonov, Aerodynamic design and experimental modeling of an innovative supersonic three-dimensional air-intake, The Aeronautical J., 2013, Vol. 117, No. 1192, P 559–584.
Yu.P. Gounko and I.I. Mazhul, Experimental characteristics of a supersonic three-dimensional air inlet with adjustable throaty, Thermophysics and Aeromechanics, 2013, Vol. 20, No. 1, P. 49–64.
Yu.P. Gounko, Supersonic inlet (with multislotted bleeding), Patent No. 2672825 RF, MPK51F02C 7/04, B64D 33/02, SPK52F02C 7/04, F64D 33/02, patent holder ITAM SB RAS, No. 2017113272; appl. 17.04.2017; publ. 19.10.2018, Bul. No. 32; priority 17.04.2917.
Yu.A. Litvinenko, V.G. Chernoray, V.V. Kozlov, L.L. Lefdal, G.R. Grek, and H. Chun, Effect of riblets on the development of the Λ-structure and its transformation to a turbulent spot, Dokl. Akad. Nauk, 2006, Vol. 407, No. 2, P. 194–197.
I.D. Zverkov and B.Yu. Zanin, Wing form effect on flow separation, Thermophysics and Aeromechanics, 2003, Vol. 10, No. 2, P. 197–204.
V.V. Bogolepov, V.N. Brazhko, L.V. Dozorova, G.I. Maikapar, and V.Yu. Neiland, Aerodynamic heating of wavy surfaces in a supersonic turbulent boundary layer, Uch. Zap. TsAGI, 1987, Vol. 18, No. 6, P. 1–7.
H.J. Brandon, R.V. Masek, and J.C. Dunavant, Aerodynamic heating to corrugation stiffened structures in thick turbulent boundary layers, AIAA J., 1975, Vol. 13, No. 11, P. 1460–1466.
Fluent 6.3. User’s Guide. Fluent Inc., Lebanon, USA, 2006.
A.A. Zheltovodov and D.D. Knight, Ideal-gas shock wave-turbulent boundary-layer interactions in supersonic flow and their modeling: three-dimensional interactions, in: Shock Wave-Boundary-Layer Interactions, H. Babinsky and J. Harvey (Ed.), 2011, P. 202–258.
I.I. Mazhul, Supersonic flow in the rectangular duct of an air inlet with the separation-induced interaction of the boundary layer with shock waves, Thermophysics and Aeromechanics, 2020, Vol. 27, No. 4, P. 507–518.
V.I. Kornilov, Three-Dimensional Near-Wall Turbulent Flows in Corner Configurations, SB RAS, Novosibirsk, 2013.
V.I. Kornilov, Correlation of the separation region length in shock wave/channel boundary layer interaction, Experiments in Fluids, 1997, No. 23, P. 489–497.
Visualization of Data of Physical and Mathematical Modeling in Gas Dynamics, V.N. Emel’yanov and K.N. Volkov (Eds.), Fizmatlit, Moscow, 2018.
K.N. Volkov, Methods of vortex flow visualization in computational fluid dynamics and their application in solving applied problems, Nauch.-Tekhn. Vest. Inform. Tekhnol., Mekh. Opt., 2014, No. 3 (91), P. 1–10.
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Mazhul, I.I. Numerical simulation of a three-dimensional flow in a channel with interaction of a plane shock wave and a longitudinally ribbed surface. Thermophys. Aeromech. 28, 487–497 (2021). https://doi.org/10.1134/S086986432104003X
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DOI: https://doi.org/10.1134/S086986432104003X