The existing computer code ARCFLO, which calculates the flow through the co
nstricted-arc heater, is modified and expanded by the use of the modern com
putational fluid dynamics technique. The entire flowfield within an are-hea
ted wind tunnel, that is, from the upstream electrode chamber to the nozzle
exit, is described by the Navier-Stokes equations, but the joule heating a
nd radiative transfer phenomena are described as in the ARCFLO code. The mo
deling of turbulence in the constrictor region is different from that in AR
CFLO. The code developed in the present work, tentatively designated as Arc
flo2, requires only the mass flow rate and electrical current as inputs and
describes the flow conditions from the upstream electrode region to the no
zzle throat. The rode reproduces the measured operating characteristics of
several wind tunnels closer than the ARCFLO code.