The flowfield induced by a single circular jet exhausting perpendicularly f
rom a flat plate into a crossflow has been investigated numerically. The fl
ow regime investigated corresponds to that encountered in a modern gas-turb
ine combustor. Reynolds-averaged solutions were obtained using a pressure-b
ased Navier-Stokes solver: The standard k-epsilon turbulence model with and
without nonequilibrium modification was employed. Two different momentum p
ur ratios, J, between the jet and the fr ee str earn are investigated, name
ly, J = 34.2 and J = 42.2. To aid the evaluation of the computational capab
ility, experimental information also has been obtained, including mean and
root-mean-square (RMS) velocity distribution downstream of the jet, and the
detailed velocity profile at the jet exit. An evaluation of the different
convection schemes reveals that the second-order upwind scheme does a notic
eably better job than the fir sf-order scheme to predict the velocity profi
le at the jet exit while predicting less mixing than the experimental measu
rement during the jet and free stream interaction. It appears that turbulen
ce modeling primarily is responsible for the deficiency the accounting for
the physics of the jet and free stream interaction.