This paper presents a model for the flow of refrigerants through adiabatic
capillary, tubes. The flow of refrigerant is characterized by a subcooled l
iquid region, a metastable liquid region, a metastable two-phase region, an
d an equilibrium two-phase region. The mass and momentum conservation equat
ions for each of these four regions are converted into finite difference fo
rms and solved using a 4th order Runge-Kutta method. The calculated results
compare well with experimental data on R-22. The predictions from the mode
l are employed to develop correlations for the design of refrigerant 134a t
hrough adiabatic capillary, tubes with the tube exit in the choked flow con
dition.