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Prikladnaya Mekhanika i Tekhnicheskaya Fizika, 2004, Volume 45, Issue 3, Pages 72–80
(Mi pmtf2380)
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This article is cited in 4 scientific papers (total in 4 papers)
Numerical simulation of a supersonic flow with transverse injection of jets
A. O. Beketaeva, A. Zh. Naimanova Institute of Mathematics at the Ministry of Education and Science, Kazakhstan, Almaty, 480100
Abstract:
A plane supersonic flow with symmetric perpendicular injection of jets through slots in the walls is numerically simulated with the use of
Navier–Stokes equations. The effect of the jet pressure ratio and Mach number on the flow structure is considered. The angle of inclination of the shock wave and the separation-region length are found as functions of the jet pressure ratio. The influence of the jet pressure ratio on the increase in the lift force arising owing to interaction of the flow with the injected jet is found.
Keywords:
supersonic flow, jet injection, Navier–Stokes equations.
Received: 03.04.2003 Accepted: 08.09.2003
Citation:
A. O. Beketaeva, A. Zh. Naimanova, “Numerical simulation of a supersonic flow with transverse injection of jets”, Prikl. Mekh. Tekh. Fiz., 45:3 (2004), 72–80; J. Appl. Mech. Tech. Phys., 45:3 (2004), 367–374
Linking options:
https://www.mathnet.ru/eng/pmtf2380 https://www.mathnet.ru/eng/pmtf/v45/i3/p72
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