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Investigation of the Flow Structure in a Model Scramjet Air Intake with Transverse Hydrogen Fuel Injection into Supersonic Crossflow
Authors:Seleznev  R K
Institution:1.Dukhov Automatics Research Institute, Moscow, Russia
;2.Ishlinsky Institute for Problems in Mechanics of the Russian Academy of Sciences, Moscow, Russia
;3.The Moscow Institute of Physics and Technology (National Research University), Dolgoprudnyi, Moscow Region, Russia
;
Abstract:Fluid Dynamics - Combustion flow inside the channel of a model scramjet air inlet with transverse hydrogen fuel injection from the bottom wall is investigated. The OH-concentration and pressure...
Keywords:
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