机构:
Joint Institute for High Temperature Russian Academy of Science,Izhorskaya str.,13/19,Moscow 125412,RussiaJoint Institute for High Temperature Russian Academy of Science,Izhorskaya str.,13/19,Moscow 125412,Russia
Sergey B.LEONOV
[1
]
Dmitry A.YARANTSEV
论文数: 0引用数: 0
h-index: 0
机构:
Joint Institute for High Temperature Russian Academy of Science,Izhorskaya str.,13/19,Moscow 125412,RussiaJoint Institute for High Temperature Russian Academy of Science,Izhorskaya str.,13/19,Moscow 125412,Russia
Dmitry A.YARANTSEV
[1
]
Anatoly P.NAPARTOVICH
论文数: 0引用数: 0
h-index: 0
机构:
StateJoint Institute for High Temperature Russian Academy of Science,Izhorskaya str.,13/19,Moscow 125412,Russia
Anatoly P.NAPARTOVICH
[2
]
Igor V.KOCHETOV
论文数: 0引用数: 0
h-index: 0
机构:
StateJoint Institute for High Temperature Russian Academy of Science,Izhorskaya str.,13/19,Moscow 125412,Russia
Igor V.KOCHETOV
[2
]
机构:
[1] Joint Institute for High Temperature Russian Academy of Science,Izhorskaya str.,13/19,Moscow 125412,Russia
Fundamental problems related to the high-speed combustion are analyzed.Theresult of plasma-chemical modeling is presented as a motivation of experimental activity.Nu-merical simulations of the effect of uniform non-equilibrium discharge on the premixed hydrogenand ethylene-air mixture in supersonic flow demonstrate an advantage of such a technique overa heating.Experimental results on multi-electrode non-uniform discharge maintenance behindwallstep and in cavity of supersonic flow are presented.The model test on hydrogen and ethyleneignition is demonstrated at direct fuel injection to low-temperature high-speed airflow.