Drh. Gillespie et al., DETAILED MEASUREMENTS OF LOCAL HEAT-TRANSFER COEFFICIENT IN THE ENTRANCE TO NORMAL AND INCLINED FILM-COOLING HOLES, Journal of turbomachinery, 118(2), 1996, pp. 285-290
The local heat transfer inside the entrance to large-scale models of f
ilm cooling holes has been measured using the transient heat transfer
technique. The method employs temperature-sensitive liquid crystals to
measure the surface temperature of large-scale perspex models. Full d
istributions of local Nusselt number were calculated based on the cool
ing passage centerline gas temperature ahead of the cooling hole. The
circumferentially averaged Nusselt number was also calculated based on
the local mixed bulk driving gas temperature to aid interpretation of
the results, and to broaden the potential application of the data. Da
ta are presented for a single film cooling hole inclined at 90 and 150
deg to the coolant duct wall. Both holes exhibited entry length heat
transfer levels that were significantly lower than those predicted by
entry length data in the presence of crossflow. The reasons for the co
mparative reduction are discussed in terms of the interpreted flow fie
ld.