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Assessment of Jet-Plate Interaction Noise Using the Lattice Boltzmann Method

机译:用格子Boltzmann方法评估喷射板相互作用噪声

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A numerical investigation of a jet interacting with a flat plate was conducted using a LBM-VLES approach. Simulations were conducted with a round jet under a large flat plate, with jet Mach number 0.3 (Re_D = 2.6 × 10~5) and 0.5 (Re_D = 4.3 × 10~3). The aim was to observe the capabilities of the method to investigate jet installation effects. Far-field SPL data were obtained using the Ffowcs-Williams and Hawkings (FW-H) surface integral method with permeable and solid surfaces. The position of the plate relative to the nozzle was varied and the effects on the far-field noise were observed. Results showed good agreement with experimental data, up to St_D = 2. Noise data obtained with solid surfaces suggested that the plate pressure field contained the main information of the installation effect. Results highlighted the potentialities of the code for investigating the noise generation from jet-surface interaction.
机译:使用LBM-VLES方法进行了与平板相互作用的射流的数值研究。在大平板下用圆形喷嘴进行模拟,喷嘴的马赫数分别为0.3(Re_D = 2.6×10〜5)和0.5(Re_D = 4.3×10〜3)。目的是观察该方法研究喷气机安装效果的能力。远场SPL数据是使用Ffowcs-Williams和Hawkings(FW-H)具有可渗透和固体表面的表面积分方法获得的。改变板相对于喷嘴的位置,并观察到对远场噪声的影响。结果表明,与St_D = 2的实验数据吻合良好。实心表面获得的噪声数据表明,板压力场包含安装效果的主要信息。结果强调了该代码用于调查喷射表面相互作用产生的噪声的潜力。

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