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NASA NTRS · 19900051235

Two-dimensional numerical simulation of a Stirling engine heat exchanger

Abstract

The first phase of an effort to develop multidimensional models of Stirling engine components is described. The ultimate goal is to model an entire engine working space. Parallel plate and tubular heat exchanger models are described, with emphasis on the central part of the channel (i.e., ignoring hydrodynamic and thermal end effects). The model assumes laminar, incompressible flow with constant thermophysical properties. In addition, a constant axial temperature gradient is imposed. The governing equations describing the model have been solved using the Crack-Nicloson finite-difference scheme. Model predictions are compared with analytical solutions for oscillating/reversing flow and heat transfer in order to check numerical accuracy. Excellent agreement is obtained for flow both in circular tubes and between parallel plates. The computational heat transfer results are in good agreement with the analytical heat transfer results for parallel plates.

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BibTeXRIS

Ibrahim, Mounir, Tew, Roy C., Dudenhoefer, James E.. 1989-01-01. Two-dimensional numerical simulation of a Stirling engine heat exchanger. https://ntrs.nasa.gov/citations/19900051235

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