Large-eddy simulation and linear acoustic modeling of entropy mode oscillations in a model combustor with coolant injection

Lean-burn combustor is particularly susceptible to combustion instability and the unsteady heat release is usually considered as the excitation of the self-maintained thermo-acoustic oscillations. The transverse coolant injection is widely used to reduce the temperature of burnt gas, but on the other hand, it will introduce temperature fluctuation inside the combustor. Therefore, it is necessary to consider the influence of the coolant injection on combustion instability, and evaluate its dynamic feature. In this paper, Large-Eddy Simulation (LES) of the self-excited pressure oscillations in a model combustor with coolant injection is carried out. The analysis of transient flow characteristics and the identification of the pressure modes confirm that one of the low frequency pressure oscillations is related to entropy fluctuations, which is known as rumble combustion instability. The LES results show that transient coolant injection is another excitation of temperature fluctuation other than unsteady combustion. The amplitude of the entropy mode oscillation increases with increasing coolant air mass whereas the change of its frequency is insignificant. According to the major feature of entropy wave oscillation caused by coolant injection, a compact coolant injection model is proposed and applied in the One Dimensional (1D) Acoustic Network Method (ANM). Key correlations used in the model match well with LES data in low frequency range. This means that the coolant injection model is a complex one reflecting the interaction of the fluctuating coolant mass, pressure and temperature. Finally, the combustion instability frequencies and modes predicted by acoustic network method are also in good agreement with LES results.     

液体火箭发动机气液同轴式喷嘴声学特性的实验研究

对液体火箭发动机气液同轴式喷嘴声学特性进行了深入的实验研究,确定了不同缩进比的气液同轴式喷嘴工作时发生啸叫的参数范围、啸叫的频率和声压级分布,并考察了啸叫对喷嘴雾化特性的影响。结果表明;气液同轴式喷嘴的啸叫区间与喷嘴的结构尺寸有密切的关系．较大的喷嘴缩进比对啸叫有明显的抑制作用,啸叫的主要成分是高频噪声,这种喷嘴啸叫可能成为诱发发动机高频不稳定燃烧的重要因素。另外,实验还发现,在较低的气体喷注压降下,啸叫对喷嘴雾化有一定的强化作用。     

大型客机舱内声学设计方案综述(一)

噪声是飞机的固有特性,舱内噪声伴随着飞机从地面开车、起飞到降落的整个旅程,严重影响乘坐舒适性。由于降噪效果的局限性,如何在设计的初始阶段,就将声学设计融入到飞机设计中显得尤为重要,也是需要长期探索和研究的问题,正是基于上述因素提出大型客机舱内声学设计方案。     

一种新型的水下地磁/声学/惯性融合导航算法

现有地磁匹配算法在水下应用中仍存在定位精度低、误匹配率高的问题。为进一步提高地磁匹配的水下定位精度,提出了一种新型的水下地磁/声学/惯性融合导航算法。首先,通过定期更新的声学测距信息对惯导指示轨迹进行刚性变换,得到粗匹配轨迹;然后,利用改进遗传算法和禁忌搜索算法对轨迹进行重构和更新,并通过卡尔曼滤波进行融合和修正,得到精匹配轨迹。仿真结果表明,所提出的算法相较于传统的ICCP算法和遗传算法能够有效提高定位精度,并且进一步降低算法的复杂度。在所提出的算法中,声学测距信息辅助发挥了提高定位精度和计算速度的作用。     

Acoustic κ-density fluctuation waves in suprathermal κ function fluids

We describe a new wave mode similar to the acoustic wave in which both density and velocity fluctuate. Unlike the acoustic wave in which the underlying distribution is Maxwellian, this new wave mode occurs when the underlying distribution is a suprathermal κ-function and involves fluctuations in the power law index, κ. This wave mode always propagates faster than the acoustic wave with an equivalent effective temperature and becomes the acoustic wave in the Maxwellian limit as κ → ∞.     

用于光纤F-P声压传感器的直流补偿解调技术研究

提出了一种改进的双腔直流补偿技术,用于解调非本征法布里-珀罗干涉(EFPI)光纤传感器,以消除腔长差与入射光波长相匹配的要求。通过消除直流分量和校准信号相位,可以从具有任意相位差的原始信号中获 得两路正交信号。通过理论仿真,制作了具有不同腔长差的EFPI光纤传感器,对所提出的方法进行了试验验证。 结果表明,该方法在解调双 F P腔 EFPI传感器时,不需要保证初始相位差恒定,且对腔长漂移不敏感,具有良好的 稳定性和实用价值。     

CFCC的几种声学参量表征方法比较

化学气相渗透(CVI)制备的CFCC的质量控制非常困难。研究该材料质量的无损检测方法对材料使用及性能表征等都具有重要意义。针对声衰减严重的问题,采用穿透法测量各声学参量,用声速、衰减、非线性等相关参量评价材料的均匀性,同时用金相法进行对比测试。结果表明:声速、衰减、非线性等参量可准确地评价材料均匀性,其中声速评价是最成熟的表征方法。     

基于数值定容弹方法的推力室阻尼特性研究

为确定推力室的声学振型频率及其阻尼特性,给出推力室最容易激发声学振型和最难衰减声学振型,建立了基于数值定容弹和半带宽法的推力室声学振型及其阻尼特性的数值模拟方法。对小推力姿轨控发动机推力室进行近圆周壁面的定容弹激励仿真,激发出了多模态的声学振型,其中,一阶切向振型为最容易激发振型,而一阶纵向振型为最难衰减振型。进一步讨论了推力室构型参数对其阻尼特性的影响,结果表明：随推力室内径增大,纵向振型得到抑制,而切向振型变得不易衰减;随推力室收缩比增加,一阶切向振型半带宽先增大后保持不变;随推力室圆柱段长度增加,各振型半带宽没有明显的变化趋势。