Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Research › peer-review
Numerical approach for the simulation of thermally non-equilibrium dissociating flows on hybrid supercomputers. / Shershnev, Anton A.; Shoev, Georgy V.; Borisov, Semyon P. et al.
19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. ed. / Fomin. Vol. 2027 American Institute of Physics Inc., 2018. 030042 (AIP Conference Proceedings; Vol. 2027).Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Research › peer-review
}
TY - GEN
T1 - Numerical approach for the simulation of thermally non-equilibrium dissociating flows on hybrid supercomputers
AU - Shershnev, Anton A.
AU - Shoev, Georgy V.
AU - Borisov, Semyon P.
AU - Kashkovsky, Alexander V.
AU - Kudryavtsev, Alexey N.
N1 - Publisher Copyright: © 2018 Author(s).
PY - 2018/11/2
Y1 - 2018/11/2
N2 - In the present work a computer code RCFS for numerical simulation of chemically reacting compressible flows on hybrid CPU/GPU supercomputers is developed. It solves 3D unsteady Euler equations for multispecies chemically reacting flows in general curvilinear coordinates using shock-capturing TVD schemes. Time advancement is carried out using the explicit Runge-Kutta TVD schemes. Program implementation uses CUDA application programming interface to perform GPU computations. Data between GPUs is distributed via domain decomposition technique. The developed code is verified on the number of test cases including supersonic flow over a cylinder.
AB - In the present work a computer code RCFS for numerical simulation of chemically reacting compressible flows on hybrid CPU/GPU supercomputers is developed. It solves 3D unsteady Euler equations for multispecies chemically reacting flows in general curvilinear coordinates using shock-capturing TVD schemes. Time advancement is carried out using the explicit Runge-Kutta TVD schemes. Program implementation uses CUDA application programming interface to perform GPU computations. Data between GPUs is distributed via domain decomposition technique. The developed code is verified on the number of test cases including supersonic flow over a cylinder.
UR - http://www.scopus.com/inward/record.url?scp=85056319057&partnerID=8YFLogxK
U2 - 10.1063/1.5065136
DO - 10.1063/1.5065136
M3 - Conference contribution
AN - SCOPUS:85056319057
VL - 2027
T3 - AIP Conference Proceedings
BT - 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018
A2 - Fomin, null
PB - American Institute of Physics Inc.
T2 - 19th International Conference on the Methods of Aerophysical Research, ICMAR 2018
Y2 - 13 August 2018 through 19 August 2018
ER -
ID: 17403750