The Influence of Large-Scale High-Intensity Turbulence on Vane Heat Transfer

Author:

Ames F. E.1

Affiliation:

1. Allison Engine Company, Indianapolis, IN 46206

Abstract

An experimental research program was undertaken to examine the influence of large-scale high-intensity turbulence on vane heat transfer. The experiment was conducted in a four-vane linear cascade at exit Reynolds numbers of 500,000 and 800,000 based on chord length. Heat transfer measurements were made for four inlet turbulence conditions including a low turbulence case (Tu ≅ 1 percent), a grid turbulence case (Tu ≅ 7.5 percent), and two levels of large-scale turbulence generated with a mock combustor at two upstream locations (Tu ≅ 12 percent and 8 percent). The heat transfer data demonstrated that the length scale, Lu, has a significant effect on stagnation region and pressure surface heat transfer.

Publisher

ASME International

Subject

Mechanical Engineering

Reference21 articles.

1. Ames, F. E., and Moffat, R. J., 1990, “Heat Transfer With High Intensity, Large Scale Turbulence: The Flat Plate Turbulent Boundary Layer and the Cylindrical Stagnation Point,” Report No. HMT-44, Thermoscience Division of Mechanical Engineering, Stanford University, CA.

2. Ames, F. E., 1994, “Experimental Study of Vane Heat Transfer and Aerodynamics at Elevated Levels of Turbulence,” NASA CR 4633.

3. Ames, F. E., and Plesniak, 1995, “The Influence of Large Scale, High Intensity Turbulence on Vane Aerodynamic Losses, Wake Growth, and Exit Turbulence Parameters,” ASME Paper No. 95-GT-290; accepted for publication in the ASME JOURNAL OF TURBOMACHINERY.

4. Arts, T., Lambert de Rouvroit, M., and Rutherford, A. W., 1990, “Aero-thermal Investigation of a Highly Loaded Transonic Linear Turbine Guide Vane Cascade,” Technical Note 174, von Karman Institute for Fluid Dynamics, Belgium.

5. Bicen A. F. , and JonesW. P., 1986, “Velocity Characteristics of Isothermal and Combusting Flows in a Model Combustor,” Combust. Sci. and Technology, Vol. 49, p. 11.

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