05 - Propulsion
EXPERIMENTAL AND NUMERICAL INVESTIGATIONS OF A SWIRL-STABILIZED JET ENGINE COMBUSTOR
B.O. Cakir¹, D. Sanned¹, P. Vauquelin¹, M. Prakash¹, J.-P. Hannappel¹, A. Subash¹, M. Richter¹, X.-S. Bai¹, C. Fureby¹; ¹Lund University, Sweden
Achieving lower global emission levels in aviation demands alternative fuels to be developed. This necessitates the characterization of thermochemical properties and combustion characteristics. Accordingly, The Triple Annular Research Swirler burner, which simulates aeroengines combustors, is employed for experimental and numerical investigations of non-reactive and reactive flows dynamics.