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Kinetic theory model for the flow of a simple gas from a two-dimensional nozzleA system of nonlinear integral equations equivalent to the Krook kinetic equation for the steady state is the mathematical basis used to develop a computer code to model the flowfields for low-thrust two-dimensional nozzles. The method of characteristics was used to solve numerically by an iteration process the approximated Boltzmann equation for the number density, temperature, and velocity profiles of a simple gas as it exhausts into a vacuum. Results predict backscatter and show the effect of the inside wall boundary layer on the flowfields external to the nozzle.
Document ID
19900050069
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Riley, B. R.
(Evansville, University IN, United States)
Scheller, K. W.
(Evansville Univ. IN, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Fluid Mechanics And Heat Transfer
Meeting Information
Meeting: Intl. Symposium on Rarefied Gas Dynamics: Space-Related Studies
Location: Pasadena, CA
Country: United States
Start Date: July 10, 1988
End Date: July 16, 1988
Accession Number
90A37124
Funding Number(s)
CONTRACT_GRANT: NAG3-746
Distribution Limits
Public
Copyright
Other

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