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Zhurnal Vychislitel'noi Matematiki i Matematicheskoi Fiziki, 2007, Volume 47, Number 2, Pages 310–320
(Mi zvmmf337)
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This article is cited in 2 scientific papers (total in 2 papers)
Numerical simulation of axisymmetric afterbody flows with jet exhaust
A. D. Savel'ev Dorodnicyn Computing Center, Russian Academy of Sciences,
ul. Vavilova 40, Moscow, 119991, Russia
Abstract:
A fifth-order accurate compact difference scheme was used to compute the flow over an axisymmetric afterbody with jet exhaust. The solution was based on the mass-averaged Navier–Stokes equations combined with
a two-parameter differential model of turbulence. The computations were performed on a specially generated mesh such that the flow in the exterior and interior of the nozzle could be described simultaneously. Numerical results are presented for various external flow conditions and various chamber pressures.
Key words:
numerical simulation, difference scheme, turbulent flows, axisymmetric boattail, propulsive jet.
Received: 30.01.2006 Revised: 25.09.2006
Citation:
A. D. Savel'ev, “Numerical simulation of axisymmetric afterbody flows with jet exhaust”, Zh. Vychisl. Mat. Mat. Fiz., 47:2 (2007), 310–320; Comput. Math. Math. Phys., 47:2 (2007), 301–310
Linking options:
https://www.mathnet.ru/eng/zvmmf337 https://www.mathnet.ru/eng/zvmmf/v47/i2/p310
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Statistics & downloads: |
Abstract page: | 324 | Full-text PDF : | 141 | References: | 40 | First page: | 1 |
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