S. A. Isaev, P. A. Baranov, A. G. Sudakov, A. E. Usachov, “Expansion of the range of critical mach numbers during control of transonic flow past a thick (20% chord) MQ airfoil with slot suction in a circular vortex flow”, Pisma v Zhurnal Tekhnicheskoi Fiziki, 2014, Volume 40, Issue 10,Pages <nobr>22

This article is cited in 6 papers

Expansion of the range of critical mach numbers during control of transonic flow past a thick (20% chord) MQ airfoil with slot suction in a circular vortex flow

S. A. Isaev^ab, P. A. Baranov^ab, A. G. Sudakov^ab, A. E. Usachov^ab

^a Saint-Petersburg State University of Civil Aviation
^b Filial of Central Aerohydrodynamic Institute

Abstract: The Navier–Stokes and Reynolds equations have been numerically solved by a factorized finite-volume method. The Reynolds equations were closed using the Menter shear-stress-transfer model modified with allowance for the curvature of flow lines. The obtained solution has been used to confirm expansion of the range of critical Mach numbers during modeling of a nonstationary flow past a thick MQ airfoil with slot suction in circular vortex cells.

Received: 25.11.2013