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One- and two-dimensional Stirling machine simulation using experimentally generated flow turbulence modelsInvestigations of one- and two-dimensional (1- or 2-D) simulations of Stirling machines centered around experimental data generated by the U. of Minnesota Mechanical Engineering Test Rig (METR) are covered. This rig was used to investigate oscillating flows about a zero mean with emphasis on laminar/turbulent flow transitions in tubes. The Space Power Demonstrator Engine (SPDE) and in particular, its heater, were the subjects of the simulations. The heater was treated as a 1- or 2-D entity in an otherwise 1-D system. The 2-D flow effects impacted the transient flow predictions in the heater itself but did not have a major impact on overall system performance. Information propagation effects may be a significant issue in the simulation (if not the performance) of high-frequency, high-pressure Stirling machines. This was investigated further by comparing a simulation against an experimentally validated analytic solution for the fluid dynamics of a transmission line. The applicability of the pressure-linking algorithm for compressible flows may be limited by characteristic number (defined as flow path information traverses per cycle); this warrants further study. Lastly the METR was simulated in 1- and 2-D. A two-parameter k-w foldback function turbulence model was developed and tested against a limited set of METR experimental data.
Document ID
19910005101
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Goldberg, Louis F.
(Minnesota Univ. Minneapolis, MN, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1990
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NAS 1.26:185285
NASA-CR-185285
Report Number: NAS 1.26:185285
Report Number: NASA-CR-185285
Accession Number
91N14414
Funding Number(s)
CONTRACT_GRANT: NAG3-693
PROJECT: RTOP 590-13-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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