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Computational heat transfer analysis for oscillatory channel flowsAn accurate finite-difference scheme has been utilized to investigate oscillatory, laminar and incompressible flow between two-parallel-plates and in circular tubes. The two-parallel-plates simulate the regenerator of a free-piston Stirling engine (foil type regenerator) and the channel wall was included in the analysis (conjugate heat transfer problem). The circular tubes simulate the cooler and heater of the engine with an isothermal wall. The study conducted covered a wide range for the maximum Reynolds number (from 75 to 60,000), Valensi number (from 2.5 to 700), and relative amplitude of fluid displacement (0.714 and 1.34). The computational results indicate a complex nature of the heat flux distribution with time and axial location in the channel. At the channel mid-plane we observed two thermal cycles (out of phase with the flow) per each flow cycle. At this axial location the wall heat flux mean value, amplitude and phase shift with the flow are dependent upon the maximum Reynolds number, Valensi number and relative amplitude of fluid displacement. At other axial locations, the wall heat flux distribution is more complex.
Document ID
19960000666
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ibrahim, Mounir
(Cleveland State Univ. OH, United States)
Kannapareddy, Mohan
(Cleveland State Univ. OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1993
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:199238
NASA-CR-199238
Report Number: NAS 1.26:199238
Report Number: NASA-CR-199238
Accession Number
96N10666
Funding Number(s)
CONTRACT_GRANT: NAG3-955
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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