Heat Transfer Measurements in an Internal Cooling System Using a Transient Technique With Infrared Thermography

Author:

Egger Christian1,Wolfersdorf Jens von2,Schnieder Martin3

Affiliation:

1. e-mail:

2. Institute of Aerospace Thermodynamics (ITLR), University of Stuttgart, Pfaffenwaldring 31, D-70569 Stuttgart, Germany

3. Alstom, Baden, CH-5401, Switzerland

Abstract

In this paper, a transient method for measuring heat transfer coefficients in internal cooling systems using infrared thermography is applied. The experiments are performed with a two-pass internal cooling channel connected by a 180 deg bend. The leading edge and the trailing edge consist of trapezoidal and nearly rectangular cross-sections, respectively, to achieve an engine-similar configuration. Within the channels, rib arrangements are considered for heat transfer enhancement. The test model is made of metallic material. During the experiment, the cooling channels are heated by the internal flow. The surface temperature response of the cooling channel walls is measured on the outer surface by infrared thermography. Additionally, fluid temperatures as well as fluid and solid properties are determined for the data analysis. The method for determining the distribution of internal heat transfer coefficients is based on a lumped capacitance approach, which considers lateral conduction in the cooling system walls as well as natural convection and radiation heat transfer on the outer surface. Because of time-dependent effects, a sensitivity analysis is performed to identify optimal time periods for data analysis. Results are compared with available literature data.

Publisher

ASME International

Subject

Mechanical Engineering

Reference27 articles.

1. Recent Studies in Turbine Blade Internal Cooling;Heat Transfer Res.,2010

2. Surface Heat Transfer From a Three-Pass Blade Cooling Passage Simulator;J. Turbomach.,1995

3. Rathjen, L., Hennecke, D. K., Sivade, C., and Semmler, K., 2002, “Detailed Experimental and Numerical Heat/Mass Transfer Investigations in a Rotating Two-Pass Coolant Channel With Staggered 45 deg Ribs,” 9th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery (ISROMAC-9).

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