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Nested subcritical flows within supercritical systemsIn supercritical systems the design inlet and outlet pressures are maintained above the thermaodynamic critical pressure P sub C. Designers rely on this simple rule of thumb to circumvent problems associated with a subcritical pressure regime nested within the supercritical pressure system along with the uncertainties in heat transfer, fluid mechanics, and thermophysical property variations. The simple rule of thumb is adequate in many low-power designs but is inadequate for high-performance turbomachines and linear systems, where nested two-phase regions can exist. Examples for a free-jet expansion with backpressure greater than P sub C and a rotor (bearing) with ambient pressure greater than P sub C illustrate the existence of subcritical pressure regimes nested within supercritical systems.
Document ID
19850013264
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hendricks, R. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Braun, M. J.
(Akron Univ. Cleveland, OH, United States)
Wheeler, R. L., III
(Akron Univ.)
Mullen, R. L.
(NASA Lewis Research Center)
Date Acquired
September 5, 2013
Publication Date
January 1, 1985
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.15:86980
NASA-TM-86980
E-2518
Report Number: NAS 1.15:86980
Report Number: NASA-TM-86980
Report Number: E-2518
Meeting Information
Meeting: Ann. Cavitation and Multiphase Flow Forum
Location: Albuquerque, NM
Country: United States
Start Date: June 24, 1985
End Date: June 26, 1985
Sponsors: American Society of Mechanical Engineers
Accession Number
85N21574
Funding Number(s)
PROJECT: RTOP 506-60-42
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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