the kinetic problem is rapidly too expensive, because it requires one computational cell per mean free path. To The aim of this paper is to introduce and validate a coupled Navier-Stokes Boltzman approach for the calculation of hypersonic overcome such difficulties, many authors have recently raref
Coupling Boltzmann and Navier–Stokes Equations by Half Fluxes
✍ Scribed by Patrick Le Tallec; François Mallinger
- Publisher
- Elsevier Science
- Year
- 1997
- Tongue
- English
- Weight
- 787 KB
- Volume
- 136
- Category
- Article
- ISSN
- 0021-9991
No coin nor oath required. For personal study only.
✦ Synopsis
a global Navier-Stokes model. At first, the coupling was achieved by imposing friction boundary conditions on the We introduce an adaptative coupling of the Boltzmann and Navier-Stokes equations to compute hypersonic flows around a vehiobstacle [4]. This coupling requires that the Boltzmann cle at high altitude. The coupling is achieved by matching half fluxes and the Navier-Stokes domains include the obstacle as at the interface of the Boltzmann and Navier-Stokes domains. The boundary, and the Navier-Stokes domain overlaps comdomains are determined automatically by computing local kinetic
pletely the Boltzmann domain. This strategy works well for residuals on a preliminary Navier-Stokes solution. Our method is developed here for monoatomic gases. Different numerical results very low Knudsen numbers but is always rather expensive.
illustrate its validity and limits. ᮊ 1997 Academic Press Moreover, rarefied effects are miscalculated by the Navier-Stokes solver when the Knudsen number increases.
📜 SIMILAR VOLUMES
We represent a new numerical method to solve the stationary Navier-Stokes equations in an unbounded domain. This technique consists in coupling the boundary integral and finite element methods. Moreover, we derive the variational formulation and well-posedness of the coupling method and provide the