Affiliation:
1. Turbine Heat Transfer Laboratory, Mechanical Engineering Department, Texas A&M University , College Station, TX 77843-3123
Abstract
Abstract
An experimental investigation of heat transfer performance in a rectangular impingement channel featuring staggered strip-fins was completed. Four configurations were considered to study the effects of varying the strip-fin height (H/d = 1.5 and 2.75) at two jet-to-target surface spacings (z/d = 3 and 6) on the heat transfer, pressure loss, and crossflow magnitude for a long impingement channel with in-line, 4 × 12 impinging jets. Also, the effect of the reference temperature choice, either jet inlet temperature or local bulk temperature, for calculating the local heat transfer coefficients was considered. The regionally averaged heat transfer coefficients were measured at seven Reynolds numbers, based on the jet diameter (10k–70k) utilizing the copper plate experimental method. The empirical correlations were expressed for the area averaged Nusselt number estimation of impingement channels with strip-fin or pin-fin roughness elements. The results showed that the long strip-fin channel with z/d = 3 provided the best thermal performance. The discharge coefficients are similar for all configurations between Rejet = 10k and 50k. The results are compared with the impingement channels with conventional pin-fins. They show that strip-fin channels provide lower pressure drop with marginally better heat transfer coefficients compared to the conventional pin-fin channels. However, when the channel weight is considered, strip-fins would increase the roughness material volume more than the conventional pin-fins.
Reference26 articles.
1. Streamwise Flow and Heat Transfer Distributions for Jet Array Impingement With Crossflow;ASME J. Heat Mass Transfer Trans. ASME,1981
2. Detailed Heat Transfer Coefficient Distributions Under an Array of Inclined Impinging Jets Using a Transient Liquid Crystal Technique
3. Impingement Heat Transfer on a Cylindrical, Concave Surface With Varying Jet Geometries;ASME J. Heat Mass Transfer-Trans. ASME,2016
4. Effect of Impingement Supply Condition on Leading Edge Heat Transfer With Rounded Impinging Jets,2012
5. Leading Edge Impingement With Racetrack-Shaped Jets and Varying Inlet Supply Conditions,2013