|
|
|
|
| LEADER |
01000caa a22002652 4500 |
| 001 |
NLM240856775 |
| 003 |
DE-627 |
| 005 |
20250217085853.0 |
| 007 |
tu |
| 008 |
231224s2014 xx ||||| 00| ||eng c |
| 028 |
5 |
2 |
|a pubmed25n0802.xml
|
| 035 |
|
|
|a (DE-627)NLM240856775
|
| 035 |
|
|
|a (NLM)25110358
|
| 040 |
|
|
|a DE-627
|b ger
|c DE-627
|e rakwb
|
| 041 |
|
|
|a eng
|
| 100 |
1 |
|
|a Coralic, Vedran
|e verfasserin
|4 aut
|
| 245 |
1 |
0 |
|a Finite-volume WENO scheme for viscous compressible multicomponent flows
|
| 264 |
|
1 |
|c 2014
|
| 336 |
|
|
|a Text
|b txt
|2 rdacontent
|
| 337 |
|
|
|a ohne Hilfsmittel zu benutzen
|b n
|2 rdamedia
|
| 338 |
|
|
|a Band
|b nc
|2 rdacarrier
|
| 500 |
|
|
|a Date Revised 21.10.2021
|
| 500 |
|
|
|a published: Print
|
| 500 |
|
|
|a Citation Status PubMed-not-MEDLINE
|
| 520 |
|
|
|a We develop a shock- and interface-capturing numerical method that is suitable for the simulation of multicomponent flows governed by the compressible Navier-Stokes equations. The numerical method is high-order accurate in smooth regions of the flow, discretely conserves the mass of each component, as well as the total momentum and energy, and is oscillation-free, i.e. it does not introduce spurious oscillations at the locations of shockwaves and/or material interfaces. The method is of Godunov-type and utilizes a fifth-order, finite-volume, weighted essentially non-oscillatory (WENO) scheme for the spatial reconstruction and a Harten-Lax-van Leer contact (HLLC) approximate Riemann solver to upwind the fluxes. A third-order total variation diminishing (TVD) Runge-Kutta (RK) algorithm is employed to march the solution in time. The derivation is generalized to three dimensions and nonuniform Cartesian grids. A two-point, fourth-order, Gaussian quadrature rule is utilized to build the spatial averages of the reconstructed variables inside the cells, as well as at cell boundaries. The algorithm is therefore fourth-order accurate in space and third-order accurate in time in smooth regions of the flow. We corroborate the properties of our numerical method by considering several challenging one-, two- and three-dimensional test cases, the most complex of which is the asymmetric collapse of an air bubble submerged in a cylindrical water cavity that is embedded in 10% gelatin
|
| 650 |
|
4 |
|a Journal Article
|
| 650 |
|
4 |
|a HLLC
|
| 650 |
|
4 |
|a WENO
|
| 650 |
|
4 |
|a interface-capturing
|
| 650 |
|
4 |
|a multicomponent flows
|
| 650 |
|
4 |
|a shock-capturing
|
| 650 |
|
4 |
|a viscous
|
| 700 |
1 |
|
|a Colonius, Tim
|e verfasserin
|4 aut
|
| 773 |
0 |
8 |
|i Enthalten in
|t Journal of computational physics
|d 1998
|g 274(2014) vom: 01. Okt., Seite 95-121
|w (DE-627)NLM098188844
|x 0021-9991
|7 nnns
|
| 773 |
1 |
8 |
|g volume:274
|g year:2014
|g day:01
|g month:10
|g pages:95-121
|
| 912 |
|
|
|a GBV_USEFLAG_A
|
| 912 |
|
|
|a SYSFLAG_A
|
| 912 |
|
|
|a GBV_NLM
|
| 912 |
|
|
|a GBV_ILN_350
|
| 951 |
|
|
|a AR
|
| 952 |
|
|
|d 274
|j 2014
|b 01
|c 10
|h 95-121
|