Louver Slot Cooling and Full-Coverage Film Cooling With a Combination Internal Coolant Supply

Author:

Click Austin1,Ligrani Phillip M.1,Hockensmith Maggie2,Knox Joseph3,Larson Chandler4,Fairbanks Avery4,Liberatore Federico5,Patel Rajeshriben5,Ho Yin-Hsiang5

Affiliation:

1. Propulsion Research Center, Department of Mechanical and Aerospace Engineering, 5000 Technology Drive, Olin B. King Technology Hall, University of Alabama in Huntsville, Huntsville, AL 35899

2. Propulsion Research Center, Department of Mechanical and Aerospace Engineering, 5000 Technology Drive, Olin B. King Technology Hall S236, University of Alabama in Huntsville, Huntsville, AL 35899

3. Propulsion Research Center, Department of Mechanical and, Aerospace Engineering, 5000 Technology Drive, Olin B. King Technology Hall S236, University of Alabama in Huntsville, Huntsville, AL 35899

4. Propulsion Research Center, Department of Mechanical, and Aerospace Engineering, 5000 Technology Drive, Olin B. King Technology Hall S236, University of Alabama in Huntsville, Huntsville, AL 35899

5. Combustion Engineering, Solar Turbines Incorporated, 2200 Pacific Highway, Mail Zone E-4, San Diego, CA 92186-5376

Abstract

Abstract Within the present investigation, a louver slot is employed upstream of an array full-coverage film cooling holes. Cooling air is supplied using a combination arrangement, with cross-flow and impingement together. The louver consists of a row of film cooling holes, contained within a specially designed device that concentrates and directs the coolant from a slot, so that it then advects as a layer downstream along the test surface. This louver-supplied coolant is then supplemented by coolant which emerges from different rows of downstream film cooling holes. The same coolant supply passage is employed for the louver row of holes, as well as for the film cooling holes, such that different louver and film cooling mass flowrates are set by different hole diameters for the two different types of cooling holes. The results are different from data provided by past investigations, because of the use and arrangement of the louver slot, and because of the unique coolant supply configurations. The experimental results are given for mainstream Reynolds numbers from 107,000 to 114,000. Full-coverage blowing ratios are constant with streamwise location along the test surface and range from 3.68 to 5.70. Corresponding louver slot blowing ratios then range from 1.72 to 2.65. Provided are heat transfer coefficient and adiabatic effectiveness distributions, which are measured along the mainstream side of the test plate. Both types of data show less variation with streamwise development location, relative to results obtained without a louver employed, when examined at the same approximate effective blowing ratio, mainstream Reynolds number, cross-flow Reynolds number, and impingement jet Reynolds number. When compared at the same effective blowing ratio or the same impingement jet Reynolds number, spanwise-averaged heat transfer coefficients are consistently lower, especially for the downstream regions of the test plate, when the louver is utilized. With the same type of comparisons, the presence of the louver slot results in significantly higher values of adiabatic film cooling effectiveness (spanwise-averaged), particularly at and near the upstream portions of the test plate. With such characteristics, dramatic increases in thermal protection are provided by the presence of the louver slot, the magnitudes of which vary with the experimental condition and test surface location.

Publisher

ASME International

Subject

Mechanical Engineering

Reference13 articles.

1. Numerical and Experimental Study of the Slot Film Cooling Jet With Various Angles;Jia,2003

2. Combined Effect of Slot Injection, Effusion Array and Dilution Hole on the Cooling Performance of a Real Combustion Liner;Ceccherini,2009

3. Combined Effect of Slot Injection, Effusion Array and Dilution Hole on the Heat Transfer Coefficient of a Real Combustor Liner Part 2: Numerical Analysis;Andreini,2010

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