A new analytical solution has been obtained for the shuttle heat trans
fer rate in displacer/cylinder systems having an axial temperature gra
dient. The temperature oscillations of both the displacer wall and the
cylinder wall were considered in the analysis. After the cyclic stead
y state solution was obtained for the temperatures of the walls by int
roducing complex temperatures, a simple mathematical expression was de
rived to calculate the shuttle heat transfer. The usefulness of the re
sults was justified by approximate solution of previous work.