Abstract
A numerical investigation of the influence of viscosity on flow around a thick airflow with vortex cells has been carried out within the framework of the multiblock approach to the solution of steady-state Reynolds equations closed using Menter's zonal model of shear-stress transfer.
This is a preview of subscription content, log in via an institution to check access.
Similar content being viewed by others
References
P. A. Baranov, S. A. Isaev, Yu. S. Prigorodov, and A. G. Sudakov, Inzh.-Fiz. Zh., 73, No. 3, 572–575 (1999).
P. A. Baranov, S. A. Isaev, Yu. S. Prigorodov, and A. G. Sudakov, Inzh.-Fiz. Zh., 73, No. 4, 719–727 (2000).
S. A. Isaev, Inzh.-Fiz. Zh., 73, No. 3, 600–605 (2000).
S. A. Isaev, S. V. Guvernyuk, M. A. Zubin, and Yu. S. Prigorodov, Inzh.-Fiz. Zh., 73, No. 2, 220–227 (2000).
S. A. Isaev, P. A. Baranov, S. V. Guvernyuk, and M. A. Zubin, Inzh.-Fiz. Zh., 75, No. 2, 3–8 (2002).
S. A. Isaev, Yu. S. Prigorodov, and A. G. Sudakov, Izv. Ross. Akad. Nauk, Mekh. Zhidk. Gaza, No. 4, 88–96 (2000).
F. R. Menter, AIAA J., 32, No. 8, 1598–1605 (1994).
I. A. Belov, S. A. Isaev, and V. A. Korobkov, Problems and Methods of Calculation of Separated Incompressible Fluid Flows [in Russian], Leningrad (1989).
S. A. Isaev, A. G. Sudakov, P. A. Baranov, and Yu. S. Prigorodov, Dokl. Ross. Akad. Nauk, 377, No. 2, 1–3 (2001). Fig. 3. Dependence of the drag coefficient (a) and the lift coefficient (b) on Re for a thick airfoil (curve 6) and its components: airfoil (1) and vortex cells (2–5); c) dependence of C y, u max c, and k max on Re. 1373
Author information
Authors and Affiliations
Rights and permissions
About this article
Cite this article
Isaev, S.A., Prigorodov, Y.S., Sudakov, A.G. et al. Numerical Simulation of the Influence of Viscosity on Turbulent Flow around a Thick Airfoil with Vortex Cells. Journal of Engineering Physics and Thermophysics 75, 1370–1373 (2002). https://doi.org/10.1023/A:1022171127699
Issue Date:
DOI: https://doi.org/10.1023/A:1022171127699