Overview of NASA Supported Stirling Thermodynamic Loss Research

929462

08/03/1992

Event
27th Intersociety Energy Conversion Engineering Conference (1992)
Authors Abstract
Content
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.
Meta TagsDetails
DOI
https://doi.org/10.4271/929462
Pages
6
Citation
Tew, R., and Geng, S., "Overview of NASA Supported Stirling Thermodynamic Loss Research," SAE Technical Paper 929462, 1992, https://doi.org/10.4271/929462.
Additional Details
Publisher
Published
Aug 3, 1992
Product Code
929462
Content Type
Technical Paper
Language
English