The present paper provides and validates a numerical procedure for the
calculation of turbulent separated Bow and heat transfer characterist
ics in axisymmetric expanding ducts, with emphasis on the annular diff
user geometry. The method is based on the fully-conserved control-volu
me representation of fully elliptic Navier-Stokes and energy equations
in body-fitted orthogonal curvilinear coordinate systems. Turbulence
is simulated via the two-equation (k-epsilon) model. The presented res
ults consist of computed velocity and streamline distributions, the ki
netic energy of turbulence and local and average Nusselt number distri
butions. Systematic variations are made in the Reynolds number (6 x 10
(3)-6 x 10(5)) and the outer wall half angles (7 degrees-20 degrees, 9
0 degrees). The study was further extended to flows with a range (0.0-
0.9) of inlet swirl number. Comparison with available experimental dat
a shows that the method with the utilized turbulence closure model and
the discretization scheme reproduces the essential features of variou
s diffuser heat transfer and fluid flow effects observed in the experi
ments. The degree of heat transfer coefficient enhancement, both maxim
um and average, increases strongly as the wall cant angle increases. T
he peak, average and exit Nusselt numbers exhibit clear dependence on
the Reynolds number and were well correlated with similar to Re-2/3, a
s was previously encountered in the literature for other types of sepa
rated regions. Although there is some indication that the exponent inc
reases to similar to 0.8 for Re > 50,000. Local heat transfer rates ha
ve been shown to increase with the increase of swirl number and to pea
k near the reattachment point.