Calculation of the Flow Structure in the Interaction with the Counterflow of a Jet Flowing from the Frontal Surface of a Body of Revolution

IF 1 4区工程技术 Q4 MECHANICS

Fluid Dynamics Pub Date : 2024-03-24 DOI:10.1134/S0015462823602681

A. V. Panasenko

引用次数: 0

Abstract

The results of the calculation of the interaction of a supersonic jet flowing at a zero angle of attack from the frontal surface of the body of rotation to the opposite supersonic flow at different supersonic Mach numbers of the flow and jet are given. The influence of the total pressure in the gas flow and in the jet on the structure of the emerging gas flow is considered.

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计算从旋转体正面流出的喷流与逆流相互作用时的流动结构

摘要本文给出了在不同超音速马赫数的气流和射流条件下，以零攻角从旋转体正面流向对面超音速气流的超音速射流相互作用的计算结果。考虑了气流和射流中的总压力对新出现的气流结构的影响。

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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来源期刊

Fluid Dynamics MECHANICS-PHYSICS, FLUIDS & PLASMAS

CiteScore

1.30

自引率

22.20%

发文量

审稿时长

6-12 weeks

期刊介绍： Fluid Dynamics is an international peer reviewed journal that publishes theoretical, computational, and experimental research on aeromechanics, hydrodynamics, plasma dynamics, underground hydrodynamics, and biomechanics of continuous media. Special attention is given to new trends developing at the leading edge of science, such as theory and application of multi-phase flows, chemically reactive flows, liquid and gas flows in electromagnetic fields, new hydrodynamical methods of increasing oil output, new approaches to the description of turbulent flows, etc.