The National Aeronautics and Space Administration (NASA) is funding research to characterize Stirling machine thermodynamic losses. NASA's primary goal is to improve Stirling design codes to support engine development for space and terrestrial power. However, much of the fundamental data is applicable to Stirling cooler and heat pump applications. The research results are reviewed. Much has been learned about oscillating-flow hydrodynamics, including laminar/turbulent transition, and tabulated data has been documented for further analysis. Now, with a better understanding of the oscillating-flow field, it is time to begin measuring the effects of oscillating flow and oscillating pressure level on heat transfer in heat exchanger flow passages and in cylinders. This critical phase of the work is just beginning.
Overview of NASA Supported Stirling Thermodynamic Loss Research
Sae Technical Papers
27th Intersociety Energy Conversion Engineering Conference (1992) ; 1992
03.08.1992
Aufsatz (Konferenz)
Englisch
NASA GRC Stirling Technology Development Overview
British Library Conference Proceedings | 2003
|Overview of NASA GRC Stirling Technology Development
AIAA | 2003
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