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Improved flammability for hydrogen fuelled scramjets with preinjection catalytic radical farming

机译:具有预注点催化自由基养殖的氢气燃料碎屑癌的可燃性改善

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Scramjet engine flight envelopes are limited to high Mach numbers due to autoignition limitations. Additionally, combustor efficiency is impacted by ignition delay times, as it directly influences the necessary combustor length. Numerical simulations using Cantera and a reduced GRI 3.0 mechanism suggest improvement of both autoignition and ignition delay times by preseeding the flow with radicals. As a nonintrusive way to produce the necessary radicals, a catalytic approach is chosen. Experimental investigations suggest a small but constant decrease in autoignition. The impact on ignition delay times is significant, but additional challenges arise due to changing flow properties with thermally driven boundary layer growth. Both improvements lag behind the numerically suggested potential, as water vapour produced in the catalytic reaction has an inhibiting effect.
机译:由于自燃限制,Scramjet发动机飞行信封仅限于高马赫数。另外,燃烧器效率受点火延迟时间影响,因为它直接影响必要的燃烧器长度。使用Cantera的数值模拟和减少的GRI 3.0机制建议通过使流动与自由基的流动改善自燃和点火延迟时间。作为产生必要的自由基的非流体方法,选择催化方法。实验调查表明自身的少但不断下降。对点火延迟时间的影响是显着的,但由于具有热驱动边界层的流动性能而导致的额外挑战产生了额外的挑战。这两种改进滞后在数值方面的潜力后面,因为在催化反应中产生的水蒸气具有抑制作用。

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