内塔对带中心体喷嘴中射流参数的影响

IF 0.5 4区 工程技术 Q4 MECHANICS Journal of Applied Mechanics and Technical Physics Pub Date : 2024-02-13 DOI:10.1134/S0021894423060160
N. P. Kiselev, I. N. Kavun, V. I. Zapryagaev, R. A. Styazhkin
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引用次数: 0

摘要

摘要 研究了一个包含中心体和塔架的轴对称喷嘴中的高速流动。确定了在\(n_{pr}= 2.25\) (\(n_{pr}\)是沉降室压力与环境压力之比)的流动状态下,主翼和附加翼的几何形状对喷嘴出口处气体动力和推力特性的影响。检测喷嘴出口处流动的方位角不均匀性。在铁塔后面的尾流中观察到了最大的方位角不均匀性。研究表明,在喷嘴导管中形成了三维跨音速气流,塔架安装在最小自由截面上;在这种气流中形成了由微弱冲击波封闭的局部超音速区域。研究发现,这种冲击波结构的形成会导致喷嘴推力降低 12%。
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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EFFECT OF INTERNAL PYLONS ON THE PARAMETERS OF THE JET FLOW IN A NOZZLE WITH A CENTRAL BODY

A high-velocity flow in an axisymmetric nozzle containing a central body and pylons is studied. The influence of the geometry of the main and additional pylons on the gas-dynamic and thrust characteristics at the nozzle exit in the flow regime with \(n_{pr}= 2.25\) (\(n_{pr}\) is the ratio of the pressure in the settling chamber to the ambient pressure) is determined. Azimuthal nonuniformity of the flow at the nozzle exit is detected. The maximum azimuthal nonuniformity is observed in the wake behind the pylons. It is shown that a three-dimensional transonic flow is formed in the nozzle duct with the pylons mounted in the minimum free cross section; local supersonic regions closed by weak shock waves are formed in this flow. It is found that the formation of such a shock wave structure is responsible for nozzle thrust reduction by 12%.

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来源期刊
CiteScore
1.20
自引率
16.70%
发文量
43
审稿时长
4-8 weeks
期刊介绍: Journal of Applied Mechanics and Technical Physics is a journal published in collaboration with the Siberian Branch of the Russian Academy of Sciences. The Journal presents papers on fluid mechanics and applied physics. Each issue contains valuable contributions on hypersonic flows; boundary layer theory; turbulence and hydrodynamic stability; free boundary flows; plasma physics; shock waves; explosives and detonation processes; combustion theory; multiphase flows; heat and mass transfer; composite materials and thermal properties of new materials, plasticity, creep, and failure.
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