Flow and thermal field measurements in a combustor simulator relevant to a gas turbine aero-engine

S. S. Vakil, K. A. Thole

Research output: Contribution to conferencePaper

4 Scopus citations

Abstract

The current demands for high performance gas turbine engines can be reached by raising combustion temperatures to increase power output. Predicting the performance of a combustor is quite challenging, particularly the turbulence levels that are generated as a result of injection from high momentum dilution jets. Prior to predicting reactions in a combustor, it is imperative that these turbulence levels can be accurately predicted. The measurements presented in this paper are of flow and thermal fields produced in a large-scale combustor simulator, which is representative of an aero-engine. Three-component laser Doppler velocimeter measurements were made to quantify the velocity field while a rake of thermocouples was used to quantify the thermal field. The results indicate large penetration depths for the high momentum dilution jets, which result in a highly turbulent flow field. As these dilution jets interact with the mainstream flow, kidney-shaped thermal fields result due to counter-rotating vortices that develop.

Original languageEnglish (US)
Pages215-224
Number of pages10
DOIs
Publication statusPublished - Dec 1 2003
Event2003 ASME Turbo Expo - Atlanta, GA, United States
Duration: Jun 16 2003Jun 19 2003

Other

Other2003 ASME Turbo Expo
CountryUnited States
CityAtlanta, GA
Period6/16/036/19/03

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All Science Journal Classification (ASJC) codes

  • Engineering(all)

Cite this

Vakil, S. S., & Thole, K. A. (2003). Flow and thermal field measurements in a combustor simulator relevant to a gas turbine aero-engine. 215-224. Paper presented at 2003 ASME Turbo Expo, Atlanta, GA, United States. https://doi.org/10.1115/GT2003-38254