涡流解析法研究对偶超音速进气口压力脉动谱的节流效应

D. A. Lyubimov
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引用次数: 0

摘要

摘要 采用旋涡解析 RANS/ILES 方法,研究了带有边界层(BL)放气系统的成对混合压缩模型超音速进气口(SAI)中的流动。分析了边界层排气系统的类型和每个 SAI 的节流对相邻 SAI 的流动特性、压力脉动水平和频谱的影响。考虑了每个 SAI 的节流方式相同和不同的情况,以及相邻 SAI 的共同和单独放气系统。简要介绍了计算方法和边界条件。根据节流程度,介绍了 SAI 中的 OASPL 水平。揭示了其中一个 SAI 的节流对邻近 SAI 的流量和 1/3 倍频程压力脉动频谱特征的影响。
本文章由计算机程序翻译,如有差异,请以英文原文为准。

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Study of the Vortex-Resolving Method of the Throttling Effect on Pressure Pulsation Spectra in a Paired Supersonic Air Intake

Abstract

Using the vortex-resolving RANS/ILES method, the flow in a paired model supersonic air intake (SAI) of mixed compression with a boundary layer (BL) bleed system is investigated. The influence of the type of BL bleed system and throttling of each of the SAI on the flow characteristics, the level and spectra of pressure pulsations in the neighboring SAIs is analyzed. Cases with the same and different throttling in each of the SAIs, as well as a common and individual bleed system for neighboring SAIs, are considered. A brief description of the calculation method and boundary conditions is given. The levels of OASPL in the SAI are presented depending on the degree of throttling. The influence of throttling of one of the SAIs on the flow and features of the 1/3-octave spectra of pressure pulsations in the neighboring SAI is revealed.

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来源期刊
Mathematical Models and Computer Simulations
Mathematical Models and Computer Simulations Mathematics-Computational Mathematics
CiteScore
1.20
自引率
0.00%
发文量
99
期刊介绍: Mathematical Models and Computer Simulations  is a journal that publishes high-quality and original articles at the forefront of development of mathematical models, numerical methods, computer-assisted studies in science and engineering with the potential for impact across the sciences, and construction of massively parallel codes for supercomputers. The problem-oriented papers are devoted to various problems including industrial mathematics, numerical simulation in multiscale and multiphysics, materials science, chemistry, economics, social, and life sciences.
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