首页> 外文会议>2003 ASME(American Society of Mechanical Engineers) Turbo Expo; Jun 16-19, 2003; Atlanta, Georgia >FORCED LOW-FREQUENCY SPRAY CHARACTERISTICS OF A GENERIC AIRBLAST SWIRL DIFFUSION BURNER
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FORCED LOW-FREQUENCY SPRAY CHARACTERISTICS OF A GENERIC AIRBLAST SWIRL DIFFUSION BURNER

机译:通用鼓风旋流扩散燃烧器的强制低频喷雾特性

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The low frequency response of the spray from a generic air-blast diffusion burner with a design typical of an engine system has been investigated as part of an experimental study to describe the combustion oscillations of aero engine combustors called rumble. The atomization process was separated from the complex instability mechanism of rumble by using sinusoidal forcing of the air mass flow rate without combustion. Pressure drop across the burner and the velocity on the burner exit were found to follow the steady Bernoulli equation. Phase-locked PIV measurements of the forced velocity field of the burner show quasi-steady behavior of the air flow field. The phase-locked spray characteristics were measured for different fuel flow rates. Here again quasi-steady behavior of the atomization process was observed. With combustion, the phase-locked Mie-scattering intensity of the spray cone was found to follow the spray behavior measured in the non-combusting tests. These findings lead to the conclusion that the unsteady droplet SMD mean and amplitude of the air-blast atomizer can be calculated using the steady state atomization correlations with the unsteady burner air velocity.
机译:作为描述用于研究航空发动机燃烧器燃烧振动(称为隆隆声)的实验研究的一部分,已经研究了具有典型发动机系统设计的通用鼓风扩散燃烧器的喷雾的低频响应。雾化过程通过使用正弦强迫空气质量流量而不燃烧而与隆隆声的复杂不稳定性机理分开。发现燃烧器上的压降和燃烧器出口上的速度遵循稳态伯努利方程。燃烧器强制速度场的锁相PIV测量显示了气流场的准稳态行为。针对不同的燃料流量测量了锁相喷雾特性。在此再次观察到雾化过程的准稳态行为。通过燃烧,发现喷雾锥的锁相米氏散射强度遵循在非燃烧测试中测得的喷雾行为。这些发现得出结论,可以使用稳态雾化与不稳定燃烧器空气速度的关系来计算鼓风雾化器的不稳定液滴S​​MD平均值和振幅。

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