Abstract

The continuing rise in turbine entry temperatures has necessitated the development of ever-more advanced cooling techniques. Effusion cooling is an example of such a system and is characterised by a high density of film cooling holes that operate at low blowing ratios, thereby achieving high overall cooling effectiveness. This paper presents both an experimental and computational investigation into the cooling performance of effusion systems. Two flat-plate geometries (with primary hole pitches of 3.0D and 5.75D) are experimentally investigated via a pressure sensitive paint technique yielding high resolution film effectiveness distributions via heat-mass transfer analogy. A computational fluid dynamics (CFD) scalar tracking method was used to model the setup computationally with the results comparing favourably to those obtained from the experiments. The CFD domain was modified to assess the cooling performance from a single film hole ejection. A superposition method was developed and applied to the resulting two-dimensional film effectiveness distribution that quickly yielded data for an array of closely-packed holes, allowing a rapid assessment of a multi-hole effusion type setup. The method produced satisfactory results at higher pitches, but at lower pitches, high levels of jet interactions reduced the performance of the superposition method.

Highlights

  • The ongoing drive to increase turbine thermal efficiency and specific power output has resulted in a continuing increase in both turbine entry temperatures (TETs) and pressure ratio

  • The results for this geometry indicate that the number of rows of holes required for fully developed films is a strong function of the blowing ratio

  • Spanwise averaged results for the multi-hole computational fluid dynamics (CFD) simulations indicate that for blowing ratios greater than 0.5, approximately seven rows of primary holes are required for fully-developed films, a value in keeping with observations made by Krewinkel [3]

Read more

Summary

Introduction

The ongoing drive to increase turbine thermal efficiency and specific power output has resulted in a continuing increase in both turbine entry temperatures (TETs) and pressure ratio. 500 K with turbine blade operating temperatures in excess of the material’s engineering limits [1]. This has necessitated increasingly complex methods of internal convective cooling on the inside of the blade surface and external film cooling, which acts to shield the blade from the hotter core gas. Effusion cooling technology presents one possible method whereby high cooling performance can be achieved whilst simultaneously reducing the required coolant flow rate. It is fundamentally based on a similar mechanism to film cooling in which coolant is passed through holes in the blade

Methods
Results
Conclusion
Full Text
Published version (Free)

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call