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Simulation of Carbon-Carbon Crack Growth Due to Carbon Oxidation in High Temperatures

机译:高温下碳氧化导致碳-碳裂纹扩展的模拟

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High-temperature gas-dynamic computational techniques are employed to study microflows in expanding cracknchannels caused by the oxidation of the channel carbon walls. Wall regression rates for three reinforced carbon–ncarbon samples that were tested in a high-enthalpy arcjet environment were modeled. The test geometries and flownconditions span flowregimes fromthe transitional through the continuum, but the samemechanismforwallmaterialnloss, atomic oxygen reaction with bare carbon, was used in all three cases. Kinetic (direct simulation Monte Carlo)nand continuum(Navier–Stokes) gas-dynamic approaches were used. The predicted wall regression rates were foundnto agree with arcjetmeasurements, and the general specimen shape change was predicted. Local gas flowfield resultsnwere found to affect the oxidation rate in amanner that cannot be predicted by previous mass loss correlations. Thenmethod holds promise for future modeling of materials gas-dynamic interactions for hypersonic flight.
机译:高温气体动力学计算技术用于研究由通道碳壁氧化引起的裂纹通道扩展中的微流。对在高焓电弧喷射环境中测试的三个增强碳-碳样品的壁回归速率进行了建模。测试的几何形状和自有条件从过渡到连续贯穿整个流态,但是在所有三种情况下都使用相同的壁材料损耗机制,即与裸碳的原子氧反应。使用动力学(直接模拟蒙特卡洛)和连续体(Navier–Stokes)气体动力学方法。发现预测的壁退化率与电弧喷射测量结果一致,并预测了总体试样形状变化。我们发现,局部气体流率的结果会影响氧化速率,而以前的质量损失相关性无法预测该结果。然后,该方法有望为高超音速飞行的材料气动力相互作用的未来建模。

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