Streamwise heat transfer variation, overall array heat transfer, and overall flow friction behavior are presented for large aspect ratio ducts containing uniformly spaced staggered arrays of circular pin fins which span the entire duct height. The array geometries investigated have short pin heights (length-to-diameter ratio of 1) and moderate spanwise (transverse) and streamwise (longitudinal) pin spacings (pitch-to-diameter ratios of 1.5 and 2.5). Such staggered array geometries are typical of applications found in internally cooled gas turbine engine airfoils. The uncovered duct walls comprise a substantial fraction of the total heat transfer area. Ten pin rows in the streamwise direction are utilized in all the experiments, with a segmented construction allowing determination of spanwise-averaged heat transfer coefficients resolved to a single row spacing in the streamwise direction. Comparisons are made with results of prior studies which are mainly restricted to flow normal to banks of circular cylinders with long length-to-diameter ratios.

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Heat transfer characteristics were measured for two-dimensional arrays of jets impinging on a surface parallel to the jet orifice plate. The impinging flow was constrained to exit in a single direction along the channel formed by the jet plate and the heat transfer surface. Both mean Nusselt numbers and streamwise Nusselt number profiles are presented as a function of Reynolds number and geometric parameters. The results show that significant periodic variations occur in the streamwise Nusselt number profiles, persisting downstream for at least ten rows of jet holes. Both channel height and hole spacing can have a significant effect on the streamwise profiles, smoothed across the periodic variations. Where significant differences exist, inline hole patterns provide better heat transfer than staggered ones, particularly downstream. These and other effects of the geometric parameters are presented and discussed.

Heat transfer characteristics were measured for inline and staggered arrays of circular jets impinging on a surface parallel to the jet orifice plate. The impinging flow was constrained to exit in a single direction along the channel formed by the jet plate and the heat transfer surface. In this configuration the air discharged from upstream transverse rows of jet holes imposes a crossflow of increasing magnitude on the succeeding downstream jet rows. Streamwise heat transfer coefficient profiles were determined for a streamwise resolution of one-third the streamwise hole spacing, utilizing a specially constructed test surface. These profiles are characterized by significant periodic variations. The downstream amplitudes are diminished by the increasing crossflow magnitude, but can persist for at least ten rows of holes. Results were obtained for streamwise hole spacings of 5, 10, and 15 hole diameters; transverse hole spacings of 4, 6, and 8 diameters; and channel heights of 1, 2, and 3 diameters. The number of transverse hole rows was fixed at ten for all configurations. The characteristics of the periodic variations are presented and discussed as a function of the geometric parameters, including the effect of hole pattern.