Abstract
The mean parameters of an incompressible equilibrium turbulent boundary layer (TBL) with zero pressure gradient (ZPG) were measured on the nozzle flat wall and on the perforated wall of the TsAGI T-128 transonic wind tunnel in the range \(Re_{\theta } = 5.3\times 10^4 - 3\times 10^5\)—velocity profiles, skin friction coefficient, and shape factor. Novel data were obtained for TBL ZPG on perforated wall in the range \(Re_{\theta } \approx 8.2\times 10^4 - 3\times 10^5\). This study supplements existing TBL ZPG data on the smooth wall at very high Reynolds numbers and enrich them by presenting novel results in the Reynolds number range \(Re_{\theta } = 2.35\times 10^5 - 2.9\times 10^5\).
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References
A.J. Smits, B.J. McKeon, I. Marusic, High-Reynolds number wall turbulence. Annu. Rev. Fluid Mech. 43(1), 353–375 (2011). https://doi.org/10.1146/annurev-fluid-122109-160753
I. Marusic, J. Monty, M. Hultmark, A. Smits, On the logarithmic region in wall turbulence. J. Fluid Mech. 716, R3 (2013). https://doi.org/10.1017/jfm.2012.511
S.A. Glazkov, A.R. Gorbushin, S.L. Osipova, A.V. Semenov, Interference of test section movable elements on its drag and flow uniformity at transonic speed. In: AIP Conference Proceedings, vol. 1770, p. 030008 (2016). https://doi.org/10.1063/1.4963950
A.R. Gorbushin, S.L. Osipova, V.B. Zametaev, Mean parameters of an incompressible turbulent boundary layer on the wind tunnel wall at very high Reynolds numbers. Flow Turbul. Combust. (2020). https://doi.org/10.1007/s10494-020-00232-z
M. Vallikivi, M. Hultmark, A.J. Smits, Turbulent boundary layer statistics at very high Reynolds number. J. Fluid Mech. 779, 371–389 (2015). https://doi.org/10.1017/jfm.2015.273
H. Nagib, K. Chauhan, P. Monkewitz, Approach to an asymptotic state for zero pressure gradient turbulent boundary layers. Philos. Trans. R. Soc. A 365 (2007). https://doi.org/10.1098/rsta.2006.1948
G.F. Oweis, E.S. Winkel, J.M. Cutbrith, S.L. Ceccio, M. Perlin, D.R. Dowling, The mean velocity profile of a smooth-flat-plate turbulent boundary layer at high Reynolds number. J. Fluid Mech. 665, 357–381 (2010). https://doi.org/10.1017/S0022112010003952
H. Fernholz, E. Krause, M. Nockemann, M. Schober, Comparative measurements in the canonical boundary layer at \(Re\theta \le 6 \times 10^4\) on the wall of the DNW. Phys. Fluids. 7, 1275–81 (1995). https://doi.org/10.1063/1.868516
V. Zametaev, A. Gorbushin, I. Lipatov, Steady secondary flow in a turbulent mixing layer. Int. J. Heat Mass Transf. 132, 655–661 (2019). https://doi.org/10.1016/j.ijheatmasstransfer.2018.12.012
P.S. Klebanoff, Z.W. Diehl, Some features of artificially thickened fully developed turbulent boundary layers with zero pressure gradient. NACA Report, vol. 1110 (1952)
J.M. Österlund, Experimental studies of zero pressure-gradient turbulent boundary-layer flow. Dissertation, Royal Institute of Technology (1999)
K.G. Winter, L. Gaudet, Turbulent Boundary-Layer Studies at High Reynolds Numbers at Mach Numbers between 0.2 and 2.8. ARC R&M 3712 London, pp. 1–57 Her Majesty’s Stationery Office (1973)
M.M. Metzger, J.C. Klewicki, A comparative study of near-wall turbulence in high and low Reynolds number boundary layers. Phys. Fluids 13, 692–701 (2001). https://doi.org/10.1063/1.1344894
L. Castillo, J. Seo, H. Hangan et al., Smooth and rough turbulent boundary layers at high Reynolds number. Exp. Fluids 36, 759 (2004). https://doi.org/10.1007/s00348-003-0758-y
T.B. Nickels, I. Marusic, S. Hafez, N. Hutchins, M.S. Chong, Some predictions of the attached eddy model for a high Reynolds number boundary layer. Philos. Trans. R. Soc. A 365(1852), 807–822 (2007). https://doi.org/10.1098/rsta.2006.1950
V.I. Kornilov, Yu.A. Litvinenko, Skin friction measurements in an incompressible turbulent boundary layer. Part 1. Adverse pressure gradient. Thermophys. Aeromech. 4, 475–491 (2001)
Acknowledgements
Experimental investigations were performed at the Central Aerohydrodynamic Institute. Data processing was funded by RFBR, project number 19-38-90296. Analysis of data and preparation of manuscript were carried out with a grant from the Russian Science Foundation (project number 20-11-20006) at MIPT.
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Gorbushin, A., Osipova, S., Zametaev, V. (2021). Mean Parameters of Incompressible Turbulent Boundary Layer with Zero Pressure Gradient on the Wall of the TsAGI T-128 Wind Tunnel at Very High Reynolds Numbers. In: Örlü, R., Talamelli, A., Peinke, J., Oberlack, M. (eds) Progress in Turbulence IX. iTi 2021. Springer Proceedings in Physics, vol 267. Springer, Cham. https://doi.org/10.1007/978-3-030-80716-0_4
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