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Studies of flows through N-sequential orificesCritical mass flux and axial pressure profile data for fluid nitrogen are presented for N = 20, 15, 10, and 7 N-sequential orifice inlet configurations uniformly spaced at 15.5 cm. These data correlate well over a wide range in reduced temperature (0.7 T sub r,o ambient) and reduced pressure (to P sub r = 2) and are in general agreement with studies of one to four inlets and labyrinth seal gas data for 33 tooth equivalent sequential inlets. Experimental and theoretical agreement is good for liquid and gas critical mass flux.
Document ID
19830010749
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hendricks, R. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1983
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-83313
E-1554
NAS 1.15:83313
Report Number: NASA-TM-83313
Report Number: E-1554
Report Number: NAS 1.15:83313
Meeting Information
Meeting: Spring Meeting of the Fluids Eng. Appl. Mech. and Bioeng. Div. of the ASME
Location: Houston, TX
Country: United States
Start Date: June 20, 1983
End Date: June 22, 1983
Accession Number
83N19020
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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