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Experiments on flow through one to four inlets of the orifice and Borda typeChoked flow rate and pressure profile data were taken on sequential axially aligned inlets of the orifice and Borda type. The configuration consisted of from two to four inlets spaced at two nominal separation distances of 0.7 and 30 diameters. At the nominal 30 diameter spacing, the reduced flow rate follows a simple empirical relation based on the reduced flow rate for a single inlet. At the nominal 0.7 diameter spacing, fluid jetting was prevalent at low temperatures and flow rates were the same as for a single inlet.
Document ID
19810021849
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hendricks, R. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Stetz, T. T.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1981
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-82680
E-963
Report Number: NASA-TM-82680
Report Number: E-963
Meeting Information
Meeting: Cryogenic Eng. Conf./Intern. Cryogenic Mater. Conf.
Location: San Diego, CA
Country: United States
Start Date: August 10, 1981
End Date: August 14, 1981
Sponsors: NBS
Accession Number
81N30391
Funding Number(s)
PROJECT: RTOP 506-53-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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