Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Research › peer-review
Modeling the interaction of a detonation wave with reactive supersonic flow using detailed chemical kinetics. / Bedarev, I. A.; Temerbekov, V. M.; Fedorov, A. V.
XV ALL-RUSSIAN SEMINAR DYNAMICS OF MULTIPHASE MEDIA. ed. / Fomin. Vol. 1939 American Institute of Physics Inc., 2018. 020002 (AIP Conference Proceedings; Vol. 1939).Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Research › peer-review
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TY - GEN
T1 - Modeling the interaction of a detonation wave with reactive supersonic flow using detailed chemical kinetics
AU - Bedarev, I. A.
AU - Temerbekov, V. M.
AU - Fedorov, A. V.
PY - 2018/3/28
Y1 - 2018/3/28
N2 - The interaction of a detonation wave with reactive supersonic flow has been studied using detailed and reduced kinetic schemes of chemical reactions in channels of various configurations: a channel with a step, a symmetric channel with a step, and a channel with a cavity. A mathematical technique based on the ANSYS/Fluent software has been developed to implement this interaction. Flow parameters are compared for various configurations and kinetic schemes. It has been shown that pulsating detonation can be used to enhance ignition in supersonic flow. The possibility of using a cavity to stabilize combustion in a supersonic combustor under the impact of a detonation wave has been demonstrated.
AB - The interaction of a detonation wave with reactive supersonic flow has been studied using detailed and reduced kinetic schemes of chemical reactions in channels of various configurations: a channel with a step, a symmetric channel with a step, and a channel with a cavity. A mathematical technique based on the ANSYS/Fluent software has been developed to implement this interaction. Flow parameters are compared for various configurations and kinetic schemes. It has been shown that pulsating detonation can be used to enhance ignition in supersonic flow. The possibility of using a cavity to stabilize combustion in a supersonic combustor under the impact of a detonation wave has been demonstrated.
KW - COMBUSTION
KW - IGNITION
UR - http://www.scopus.com/inward/record.url?scp=85045142134&partnerID=8YFLogxK
U2 - 10.1063/1.5027314
DO - 10.1063/1.5027314
M3 - Conference contribution
AN - SCOPUS:85045142134
VL - 1939
T3 - AIP Conference Proceedings
BT - XV ALL-RUSSIAN SEMINAR DYNAMICS OF MULTIPHASE MEDIA
A2 - Fomin, null
PB - American Institute of Physics Inc.
T2 - 15th All-Russian Seminar on Dynamics of Multiphase Media, DMM 2017
Y2 - 3 October 2017 through 5 October 2017
ER -
ID: 12438999