Direct Numerical Simulation of the Turbulent Flow Laminarization in a Pipe at Re = 5000

Author:

Zaripov D. I.,Ivashchenko V. A.,Panteleev S. A.,Luk’yanov A. A.,Mullyadzhanov R. I.

Publisher

Allerton Press

Reference16 articles.

1. Koval’nogov, N.N. and Khakhaleva, L.V., Turbulent Flow and Friction Resistance in a Perforated Pipe with Damping Cavities, Izv. Vuz. Av. Tekhnika, 2002, no. 3, pp. 19–21. [Russian Aeronautics (Engl.Transl.), 2002. no. 3, pp. 25–29].

2. Bondarenko, A.A., Kovrizhnykh, E.N., and Koval’nogov, N.N., Laminarization of a Boundary Layer on the Perforated Surface with Blind Damping Cavities in an Accelerating Flow, Izv. Vuz. Av. Tekhnika, 2011, vol. 54, no. 11, pp. 41–44 [Russian Aeronautics (Engl. Transl.), vol. 54, no. 1, pp. 56–61].

3. Anisimova, I.V., Gortyshov, Yu.F., and Ignat’ev, V.N., On a Problem of Reducing the Hydrodynamic Drag in the Pipelines of Power Plants, Izv. Vuz. Av. Tekhnika, 2016, vol. 59, no. 3, pp. 111–115 [Russian Aeronautics (Engl. Transl.), vol. 59, no. 3, pp. 414–418].

4. Boiko, A.V. and Kornilov, V.I., On the Vertical Large Eddy Breakup Device Capability to Decrease the Turbulent Drag, Teplofizika i Aeromekhanika, 2009, vol. 16, no. 4, pp. 583–596 [Thermophysics and Aeromechanics (Engl. Transl.), vol. 16, no. 4, pp. 549–560].

5. Kornilov, V.I., Control of Turbulent Boundary Layer on a Wing Section by Combined Blowing/Suction, Teplofizika i Aeromekhanika, 2018, vol. 25, no. 2, pp. 163–176 [Thermophysics and Aeromechanics (Engl. Transl.), vol. 25, no. 2, pp. 155–167].

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