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Measurement and analysis of a small nozzle plume in vacuumPitot pressures and flow angles are measured in the plume of a nozzle flowing nitrogen and exhausting to a vacuum. Total pressures are measured with Pitot tubes sized for specific regions of the plume and flow angles measured with a conical probe. The measurement area for total pressure extends 480 mm (16 exit diameters) downstream of the nozzle exit plane and radially to 60 mm (1.9 exit diameters) off the plume axis. The measurement area for flow angle extends to 160 mm (5 exit diameters) downstream and radially to 60 mm. The measurements are compared to results from a numerical simulation of the flow that is based on kinetic theory and uses the direct-simulation Monte Carlo (DSMC) method. Comparisons of computed results from the DSMC method with measurements of flow angle display good agreement in the far-field of the plume and improve with increasing distance from the exit plane. Pitot pressures computed from the DSMC method are in reasonably good agreement with experimental results over the entire measurement area.
Document ID
19930017372
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Penko, P. F.
(NASA Lewis Research Center Cleveland, OH, United States)
Boyd, I. D.
(Eloret Corp. Moffett Field, CA., United States)
Meissner, D. L.
(Toledo Univ. OH., United States)
Dewitt, K. J.
(Toledo Univ. OH., United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1993
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-7383
AIAA PAPER 92-3108
NAS 1.15:106066
NASA-TM-106066
Meeting Information
Meeting: Joint Propulsion Conference and Exhibit
Location: Nashville, TN
Country: United States
Start Date: July 6, 1992
End Date: July 8, 1992
Sponsors: AIAA, ASME, SAE, ASEE
Accession Number
93N26561
Funding Number(s)
PROJECT: RTOP 506-42-31
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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