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Low-Density Nozzle Flow by the Direct Simulation Monte Carlo and Continuum MethodsTwo different approaches, the direct simulation Monte Carlo (DSMC) method based on molecular gasdynamics, and a finite-volume approximation of the Navier-Stokes equations, which are based on continuum gasdynamics, are employed in the analysis of a low-density gas flow in a small converging-diverging nozzle. The fluid experiences various kinds of flow regimes including continuum, slip, transition, and free-molecular. Results from the two numerical methods are compared with Rothe's experimental data, in which density and rotational temperature variations along the centerline and at various locations inside a low-density nozzle were measured by the electron-beam fluorescence technique. The continuum approach showed good agreement with the experimental data as far as density is concerned. The results from the DSMC method showed good agreement with the experimental data, both in the density and the rotational temperature. It is also shown that the simulation parameters, such as the gas/surface interaction model, the energy exchange model between rotational and translational modes, and the viscosity-temperature exponent, have substantial effects on the results of the DSMC method.
Document ID
19970009863
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Chung, Chang-Hong
(NASA Lewis Research Center Cleveland, OH United States)
Kim, Sku C.
(NYMA, Inc. Cleveland, OH United States)
Stubbs, Robert M.
(NASA Lewis Research Center Cleveland, OH United States)
Dewitt, Kenneth J.
(Toledo Univ. OH United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1994
Publication Information
Publication: Journal of Propulsion and Power
Publisher: American Institute of Aeronautics and Astronautics, Inc.
Volume: 11
Issue: 1
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-203335
Paper 93-0727
NAS 1.26:203335
Meeting Information
Meeting: Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 11, 1993
End Date: January 14, 1993
Accession Number
97N15231
Funding Number(s)
CONTRACT_GRANT: NAS3-25266
CONTRACT_GRANT: NAS3-171
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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