NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Numerical simulation of rarefied gas flow through a slitTwo different approaches, the finite-difference method coupled with the discrete-ordinate method (FDDO), and the direct-simulation Monte Carlo (DSMC) method, are used in the analysis of the flow of a rarefied gas from one reservoir to another through a two-dimensional slit. The cases considered are for hard vacuum downstream pressure, finite pressure ratios, and isobaric pressure with thermal diffusion, which are not well established in spite of the simplicity of the flow field. In the FDDO analysis, by employing the discrete-ordinate method, the Boltzmann equation simplified by a model collision integral is transformed to a set of partial differential equations which are continuous in physical space but are point functions in molecular velocity space. The set of partial differential equations are solved by means of a finite-difference approximation. In the DSMC analysis, three kinds of collision sampling techniques, the time counter (TC) method, the null collision (NC) method, and the no time counter (NTC) method, are used.
Document ID
19900051342
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Keith, Theo G., Jr.
(Toledo Univ. OH, United States)
Jeng, Duen-Ren
(Toledo Univ. OH, United States)
De Witt, Kenneth J.
(Toledo, University OH, United States)
Chung, Chan-Hong
(Toledo Univ. OH, United States)
Date Acquired
August 14, 2013
Publication Date
June 1, 1990
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 90-1694
Accession Number
90A38397
Funding Number(s)
CONTRACT_GRANT: NAG3-577
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available