Результаты исследований: Публикации в книгах, отчётах, сборниках, трудах конференций › статья в сборнике материалов конференции › научная › Рецензирование
Numerical simulation of detonation propagation in a plane channel with detailed chemical mechanisms on supercomputers with GPUs. / Borisov, S. P.; Kudryavtsev, A. N.; Shershnev, A. A.
19th International Conference on the Methods of Aerophysical Research, ICMAR 2018. ред. / Fomin. Том 2027 American Institute of Physics Inc., 2018. 040023 (AIP Conference Proceedings; Том 2027).Результаты исследований: Публикации в книгах, отчётах, сборниках, трудах конференций › статья в сборнике материалов конференции › научная › Рецензирование
}
TY - GEN
T1 - Numerical simulation of detonation propagation in a plane channel with detailed chemical mechanisms on supercomputers with GPUs
AU - Borisov, S. P.
AU - Kudryavtsev, A. N.
AU - Shershnev, A. A.
N1 - Publisher Copyright: © 2018 Author(s).
PY - 2018/11/2
Y1 - 2018/11/2
N2 - In this work we present the preliminary results of numerical simulations of detonation wave propagation in a plane channel conducted with an in-home code solving the chemically reacting Euler equations on supercomputers with GPUs. The simulations are performed with four detailed chemical kinetics mechanisms (ONERA, Deiterding, modified Jachimowski, Peterson and Hanson models). The latter model includes a pressure-dependent reaction. The 1D and 2D Euler equations are solved for a hy-drogen/oxygen mixture using high-order shock-capturing TVD schemes and a finite-rate chemistry solver. The sizes of detonation cells obtained with different models are compared.
AB - In this work we present the preliminary results of numerical simulations of detonation wave propagation in a plane channel conducted with an in-home code solving the chemically reacting Euler equations on supercomputers with GPUs. The simulations are performed with four detailed chemical kinetics mechanisms (ONERA, Deiterding, modified Jachimowski, Peterson and Hanson models). The latter model includes a pressure-dependent reaction. The 1D and 2D Euler equations are solved for a hy-drogen/oxygen mixture using high-order shock-capturing TVD schemes and a finite-rate chemistry solver. The sizes of detonation cells obtained with different models are compared.
UR - http://www.scopus.com/inward/record.url?scp=85056333794&partnerID=8YFLogxK
U2 - 10.1063/1.5065297
DO - 10.1063/1.5065297
M3 - Conference contribution
AN - SCOPUS:85056333794
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: 17403335