Hostname: page-component-78c5997874-m6dg7 Total loading time: 0 Render date: 2024-11-07T09:52:30.970Z Has data issue: false hasContentIssue false

Nearly free-molecular slit flow at finite pressure and temperature ratios

Published online by Cambridge University Press:  29 March 2006

P. Y. Wang
Affiliation:
Department of Mechanical Engineering and Astronautical Science, Northwestern University Permanent address: Chung-Shan Institute of Science and Technology, Taipei, Taiwan, The Republic of China.
E. Y. Yu
Affiliation:
Department of Mechanical Engineering and Astronautical Science, Northwestern University

Abstract

An analytical study is made of nearly free-molecular flow of a noble gas from one reservoir to another through a two-dimensional slit, with finite pressure and temperature ratios across the slit. The fundamental solution of the linear Boltzmann equation is employed in the study. The total mass flow is calculated to the first-order correction terms, of the order of α ln α and α, where α is the inverse Knudsen number. The coefficients of these terms are in general multiple integrals, but they become explicit functions of the pressure and temperature ratios after the multiple integrations are carried out by using Krook collision model. When the general result is simplified to the isothermal case the first-order correction has a negative value, indicating the reduction of the total mass flow due to intermolecular collisions in the counter flows.

Type
Research Article
Copyright
© 1971 Cambridge University Press

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

Bhatnager, P. L., Gross, E. P. & Krook, M. 1954 Phys. Rev. 94, 511.
Chapman, S. & Cowling, T. G. 1960 The Mathematical Theory of Non-Uniform Gases, chap. 7. Cambridge University Press.
Grad, H. 1959 In Proc. Symp. on Aerodynamics of Upper Atmosphere, Project Rand.
Grad, H. 1963 In Rarefied Gas Dynamics, vol. 1 (ed. J. A. Laurmann) p. 26. Academic.
Knudsen, M. 1909 Ann. Phys. 28, 75.
Liepmann, H. W. 1961 J. Fluid Mech. 10, 65.
Lord, R. G., Hurlbut, F. C. & Willis, D. R. 1967 In Rarefied Gas Dynamics, vol. 2 (ed. C. L. Brundin) p. 1235. Academic.
Narasimha, R. 1961 J. Fluid Mech. 10, 371.
Rotenberg, A. & Weitzner, H. 1969 Phys. Fluids, 12, 1573.
Smetana, F. O., Sherrill, W. A. & Schort, D. R. 1967 In Rarefied Gas Dynamics, vol. 2 (ed. C. L. Brundin) p. 1243. Academic.
Sreekanth, A. K. 1965 In Rarefied Gas Dynamics, vol. 1 (ed. J. H. de Leeuw) p. 621. Academic.
Stewart, J. D. 1969 J. Fluid Mech. 35, 599.
Willis, D. R. 1958 Princeton University Aeronaut. Eng. Rep. no. 442.
Willis, D. R. 1965 J. Fluid Mech. 21, 21.
Yu, E. Y. 1967 Phys. Fluids, 10, 2466.