Behaviour of small regions of different gases carried in accelerated gas flows

Author:

Rudinger George,Somers Lowell M.

Abstract

Small regions in a flow where the density is different from that of the surrounding gas do not exactly follow accelerated motions of the latter, but move faster or slower depending on whether their density is smaller or larger than that of the main flow. This behaviour cannot be quantitatively explained by treating a gas ‘bubble’ as a hypothetical solid particle of the same density, because a gas bubble cannot move relative to the surrounding gas without being transformed into a vortex which absorbs part of the energy of the relative motion.To illustrate the acceleration effect, the flow velocity behind known pressure waves in a shock tube is compared with the observed velocity of a bubble produced by a spark discharge. The displacement of such a bubble by a wave exceeds that of a flow element by more than 20%, but the bubble density is not known. If the spark discharge is replaced by a small jet of another gas, a pressure wave cuts off a section of this jet which then represents a bubble of known density.A theory is developed which permits computing the response of such bubbles to accelerations. The ratio of the bubble velocity to the velocity of the surrounding gas depends on the density ratio for the two gases and on the shape of the bubble, but not on the acceleration. Experimental results with H2, He, and SF6bubbles in air, accelerated by shock waves of various strength, are presented and agree well with the theoretical predictions. The results apply regardless of whether accelerations are produced by pressure waves in a non-steady flow or by curvature of streamlines in a steady flow. Various aspects of the experimental observations are discussed.

Publisher

Cambridge University Press (CUP)

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Reference17 articles.

1. Birkhoff, G. & Caywood, T. E. 1949 Fluid flow patterns. J. Appl. Phys. 20,646.

2. Wright, F. H. 1951 The particle-track method of tracing fluid streamlines. Jet Propulsion Lab., Calif. Inst. of Technology, Progress Rept, no. 3–23.

3. Markstein, G. H. 1957 A shock tube study of flame front-pressure wave interaction.6th Symposium (International) on Combustion, pp.387–98.New York:Reinhold.

4. Hirschfelder, J. O. , Curtis, C. F. & Bird, R. B. 1954 Molecular Theory of Gases and Liquids .New York:Wiley.

5. Saheki, Y. 1947 On the measurement of wind (tunnel) velocity (distributions) by the electric spark method. Hokkaido Univ., Faculty of Engineering Memoirs , 8, 185; transl. by E. Hope, Nat. Res. Counc. Can. Tech. Trans. TT-100 (1950).

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3