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NASA NTRS ยท 19830046054

Computation techniques and computer programs to analyze Stirling cycle engines using characteristic dynamic energy equations

Abstract

The basic equations that are used to describe the physical phenomena in a Stirling cycle engine are the general energy equations and equations for the conservation of mass and conversion of momentum. These equations, together with the equation of state, an analytical expression for the gas velocity, and an equation for mesh temperature are used in this computer study of Stirling cycle characteristics. The partial differential equations describing the physical phenomena that occurs in a Stirling cycle engine are of the hyperbolic type. The hyperbolic equations have real characteristic lines. By utilizing appropriate points along these curved lines the partial differential equations can be reduced to ordinary differential equations. These equations are solved numerically using a fourth-fifth order Runge-Kutta integration technique.

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BibTeXRIS

Larson, V. H.. 1982-01-01. Computation techniques and computer programs to analyze Stirling cycle engines using characteristic dynamic energy equations. https://ntrs.nasa.gov/citations/19830046054

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