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Simulation of Low-density Nozzle Plumes in Non-zero Ambient PressuresThe direct simulation Monte-Carlo (DSMC) method was applied to the analysis of low-density nitrogen plumes exhausting from a small converging-diverging nozzle into finite ambient pressures. Two cases were considered that simulated actual test conditions in a vacuum facility. The numerical simulations readily captured the complicated flow structure of the overexpanded plumes adjusting to the finite ambient pressures, including Mach disks and barrel shaped shocks. The numerical simulations compared well to experimental data of Rothe.
Document ID
19940028236
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chung, Chan-Hong
(Toledo Univ. OH., United States)
Dewitt, Kenneth J.
(Toledo Univ. OH., United States)
Stubbs, Robert M.
(NASA Lewis Research Center Cleveland, OH, United States)
Penko, Paul F.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1994
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.15:106501
AIAA PAPER 94-0357
NASA-TM-106501
E-8514
Meeting Information
Meeting: Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 10, 1994
End Date: January 13, 1994
Sponsors: AIAA
Accession Number
94N32742
Funding Number(s)
CONTRACT_GRANT: NCC3-171
PROJECT: RTOP 505-62-52
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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