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Experimental and Numerical Study of High-Altitude Ignition of a Turbojet Combustor

机译:涡轮喷气燃烧器高空点火的实验与数值研究

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摘要

This paper aims at contributing to the methodology used for the numerical prediction of ignition inside a combustion chamber. For this purpose, experiments are carried out in a model combustor with improved optical access. Laser tomography and high-speed video give a first insight of the unsteady airflow and the flame structure. Laser Doppler Anemometry is used to measure the gas flow velocity field, and the non-reactive two-phase flow is studied in detail using Particle Doppler Analysis. The velocity field of the burning spray is measured using Particle Image Velocimetry. Ignition tests are performed to evaluate the minimum global equivalence ratio.udThis in-depth database is used to validate RANS simulations conducted in parallel using ONERA CFD code CEDRE. The numerical model for transient, spherical kernel ignition, proposed in previous work, has been improved and fully implemented in CEDRE. A first parametric study on a basic configuration has been partially validated for gaseous, monodisperse and polydisperse two-phase mixtures, and gives a better understanding of the first stages of flame propagation. This model is then used in combination with CEDRE to estimate the ignition probability of given spark- plug positions in the model combustor.
机译:本文旨在为用于燃烧室内点火数值预测的方法做出贡献。为此,在具有改进的光学通道的模型燃烧器中进行实验。激光层析成像和高速视频使人们对不稳定的气流和火焰结构有了初步了解。使用激光多普勒风速仪测量气体流速场,并使用粒子多普勒分析对非反应性两相流进行了详细研究。使用粒子图像测速仪测量燃烧喷雾的速度场。进行点火测试以评估最小的总体当量比。 ud此深度数据库用于验证使用ONERA CFD代码CEDRE并行执行的RANS仿真。在先前的工作中提出的瞬态球核点火的数值模型已得到改进,并已在CEDRE中完全实现。对基本构型的首次参数研究已部分验证了气态,单分散和多分散两相混合物的情况,使人们对火焰传播的第一阶段有了更好的了解。然后将此模型与CEDRE结合使用,以估计模型燃烧器中给定火花塞位置的点火概率。

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