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The mechanism of self-ignition and flame holding in supersonic combustion chamber

机译:超音速燃烧室自燃和火焰持有的机理

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The presented research has been concentrated to definition of conditions of self-ignition of hydrogen in the combustion chamber at the entrance Mach number 4. The experimental model was made in the form of rectangular channel with a flame holder in the form of backward facing step (BFS). Fuel injection was carried out in front of BFS on the top and bottom walls of model through 8 circular holes, which was located under angles of 45° or 90°. Performed investigations allowed determining effective model of fuel injection for self-ignition and flame stabilization and prevention of choking of the channel. It is shown that the choice of the fuel injection scheme determines the ignition conditions and controlling the combustion process.
机译:本研究的研究已经集中于在入口马赫的燃烧室中氢气的自点火条件的定义。实验模型以矩形通道的形式,具有落后步骤的形式的火焰保持器( BFS)。燃料喷射在模型的顶部和底壁上在模型的顶部和底壁上进行,该圆孔位于45°或90°的角度下。进行的调查允许确定燃料喷射的有效模型,用于自点火和火焰稳定,并防止通道的窒息。结果表明,燃料喷射方案的选择决定了点火条件并控制燃烧过程。

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