| 000 | 02324nam a2200361 i 4500 | ||
|---|---|---|---|
| 001 | CR9781108877534 | ||
| 003 | UkCbUP | ||
| 005 | 20230516164909.0 | ||
| 006 | m|||||o||d|||||||| | ||
| 007 | cr|||||||||||| | ||
| 008 | 191014s2021||||enk o ||1 0|eng|d | ||
| 020 | _a9781108877534 (ebook) | ||
| 020 | _z9781108792486 (paperback) | ||
| 040 |
_aUkCbUP _beng _erda _cUkCbUP |
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| 050 | 4 |
_aTL570 _b.X9 2021 |
|
| 082 | 0 | 4 |
_a629.1323 _223 |
| 100 | 1 |
_aXu, Kun, _eauthor. _967996 |
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| 245 | 1 | 2 |
_aA unified computational fluid dynamics framework from rarefied to continuum regimes / _cKun Xu. |
| 264 | 1 |
_aCambridge : _bCambridge University Press, _c2021. |
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| 300 |
_a1 online resource (97 pages) : _bdigital, PDF file(s). |
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| 336 |
_atext _btxt _2rdacontent |
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| 337 |
_acomputer _bc _2rdamedia |
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| 338 |
_aonline resource _bcr _2rdacarrier |
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| 490 | 0 |
_aCambridge elements. Elements in Aerospace Engineering, _x2631-7850 |
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| 500 | _aTitle from publisher's bibliographic system (viewed on 31 May 2021). | ||
| 520 | _aThis Element presents a unified computational fluid dynamics framework from rarefied to continuum regimes. The framework is based on the direct modelling of flow physics in a discretized space. The mesh size and time step are used as modelling scales in the construction of discretized governing equations. With the variation-of-cell Knudsen number, continuous modelling equations in different regimes have been obtained, and the Boltzmann and Navier-Stokes equations become two limiting equations in the kinetic and hydrodynamic scales. The unified algorithms include the discrete velocity method (DVM)-based unified gas-kinetic scheme (UGKS), the particlebased unified gas-kinetic particle method (UGKP), and the wave and particle-based unified gas-kinetic wave-particle method (UGKWP). The UGKWP is a multi-scale method with the particle for non-equilibrium transport and wave for equilibrium evolution. The particle dynamics in the rarefied regime and the hydrodynamic flow solver in the continuum regime have been unified according to the cell's Knudsen number. | ||
| 650 | 0 |
_aAerodynamics. _98123 |
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| 650 | 0 |
_aAerospace engineering. _96033 |
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| 650 | 0 |
_aFluid dynamics. _94077 |
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| 776 | 0 | 8 |
_iPrint version: _z9781108792486 |
| 856 | 4 | 0 | _uhttps://doi.org/10.1017/9781108877534 |
| 942 | _cEBK | ||
| 999 |
_c82203 _d82203 |
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