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Pressure measurements in a low-density nozzle plume for code verificationMeasurements of Pitot pressure were made in the exit plane and plume of a low-density, nitrogen nozzle flow. Two numerical computer codes were used to analyze the flow, including one based on continuum theory using the explicit MacCormack method, and the other on kinetic theory using the method of direct-simulation Monte Carlo (DSMC). The continuum analysis was carried to the nozzle exit plane and the results were compared to the measurements. The DSMC analysis was extended into the plume of the nozzle flow and the results were compared with measurements at the exit plane and axial stations 12, 24 and 36 mm into the near-field plume. Two experimental apparatus were used that differed in design and gave slightly different profiles of pressure measurements. The DSMC method compared well with the measurements from each apparatus at all axial stations and provided a more accurate prediction of the flow than the continuum method, verifying the validity of DSMC for such calculations.
Document ID
19910019914
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Penko, Paul F.
(NASA Lewis Research Center Cleveland, OH., United States)
Boyd, Iain D.
(Eloret Corp. Moffett Field, CA., United States)
Meissner, Dana L.
(Toledo Univ. OH., United States)
Dewitt, Kenneth J.
(Toledo Univ. OH., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-6463
AIAA PAPER 91-2110
NAS 1.15:105170
NASA-TM-105170
Report Number: E-6463
Report Number: AIAA PAPER 91-2110
Report Number: NAS 1.15:105170
Report Number: NASA-TM-105170
Meeting Information
Meeting: Joint Propulsion Conference
Location: Sacramento, CA
Country: United States
Start Date: June 24, 1991
End Date: June 27, 1991
Sponsors: ASEE, ASME, AIAA, SAE
Accession Number
91N29228
Funding Number(s)
PROJECT: RTOP 506-42-31
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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