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Jan 2007

Volume 19, Issue 1, Articles (01xxxx)

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back to top Compressible Flows

Multiple-temperature kinetic model for continuum and near continuum flows

Kun Xu, Hongwei Liu, and Jianzheng Jiang

Phys. Fluids 19, 016101 (2007); http://dx.doi.org/10.1063/1.2429037 (12 pages) | Cited 11 times

Online Publication Date: 11 January 2007

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A gas-kinetic model with multiple translational temperature for the continuum and near continuum flow simulations is proposed. The main purpose for this work is to derive the generalized Navier-Stokes equations with multiple temperature. It is well recognized that for increasingly rarefied flowfields, the predictions from continuum formulation, such as the Navier-Stokes equations lose accuracy. These inaccuracies may be partially due to the single temperature assumption in the standard Navier-Stokes equations. Here, based on an extended Bhatnagar-Gross-Krook (BGK) model with multiple translational temperature, the numerical scheme for its corresponding Navier-Stokes equations is also constructed. In the current approach, the energy exchange between x, y, and z directions is modeled through the particle collision, and individual energy equation in different direction is obtained. The kinetic model, newly constructed is an enlarged system in comparison with Holway’s ellipsoid statistical BGK model (ES-BGK). The detailed difference is presented in this paper. In the newly derived “Navier-Stokes” equations from the current model, all viscous terms are replaced by the temperature relaxation terms. The relation between the stress and strain in the standard Navier-Stokes equations is recovered only in the limiting case when the flow is close to the equilibrium, such as small temperature differences in different directions. In order to validate the generalized Navier-Stokes equations, we apply them to the study of Couette and Poiseuille flows with a wide range of Knudsen numbers. In the continuum flow regime, the standard Navier-Stokes solutions are precisely recovered. In the near continuum flow regime, the simulation results are compared with the direct simulation Monte Carlo solutions. The anomalous phenomena in the pressure and temperature distributions from the standard Navier-Stokes equations in the Poiseuille flow case at Kn = 0.1 are well resolved by the generalized Navier-Stokes equations. This paper clearly shows that many thermal nonequilibrium phenomena in the near continuum flow regime can be well captured by modifying some assumptions in the standard Navier-Stokes equations.
Show PACS
47.45.Ab Kinetic theory of gases
47.10.ad Navier-Stokes equations
47.15.Rq Laminar flows in cavities, channels, ducts, and conduits
47.60.-i Flow phenomena in quasi-one-dimensional systems
47.70.Nd Nonequilibrium gas dynamics
51.10.+y Kinetic and transport theory of gases

Strong interaction of a turbulent spot with a shock-induced separation bubble

L. Krishnan and N. D. Sandham

Phys. Fluids 19, 016102 (2007); http://dx.doi.org/10.1063/1.2432158 (11 pages) | Cited 5 times

Online Publication Date: 25 January 2007

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Direct numerical simulations have been conducted to study the passage of a turbulent spot through a shock-induced separation bubble. Localized blowing is used to trip the boundary layer well upstream of the shock impingement, leading to mature turbulent spots at impingement, with a length comparable to the length of the separation zone. Interactions are simulated at free stream Mach numbers of two and four, for isothermal (hot) wall boundary conditions. The core of the spot is seen to tunnel through the separation bubble, leading to a transient reattachment of the flow. Recovery times are long due to the influence of the calmed region behind the spot. The propagation speed of the trailing interface of the spot decreases during the interaction and a substantial increase in the lateral spreading of the spot was observed. A conceptual model based on the growth of the lateral shear layer near the wingtips of the spot is used to explain the change in lateral growth rate.
Show PACS
47.27.nb Boundary layer turbulence
47.40.Nm Shock wave interactions and shock effects
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