@conference {Vaz2004511,
	title = {On the stability range of a cylindrical combustor for operation in the flox regime},
	booktitle = {Proceedings of the ASME Turbo Expo 2004},
	volume = {1},
	year = {2004},
	note = {<p>cited By 2</p>
},
	pages = {511-516},
	abstract = {<p>The implementation of flameless combustion in gas turbines is a recent research topic motivated by the potential for ultra-low NO x emissions and improvement of the combustion acoustics. This paper presents preliminary results of the implementation of flameless oxidation in a laboratory model of a cylindrical combustor (in view of stationary and micro gas turbines). Guidelines are given for the start-up of this combustion system. The experimental study then assesses, for atmospheric conditions, the combined effect of the air-to-fuel ratio, wall temperature and jet velocity on combustion stability. Global volumetric heat releases up to 16 MW/m 3, and air preheat up to 265 {\textdegree}C are attained. The numerical simulations give insight into the recirculating pattern of the flow and the state of mixing of reactants and products in the near-nozzle region. The turbulence-chemistry interaction is accounted for by means of the non-premixed flamelet-PDF approach (including finite rate chemistry and scalar dissipation rates up to the extinction limit).</p>
},
	url = {http://www.scopus.com/inward/record.url?eid=2-s2.0-10244257664\&partnerID=40\&md5=7263c084938c02d818b510e4e5f4f7e9},
	author = {Vaz, D.C.a b , Van Buijtenen, J.P.a , Borges, A.R.J.b , Spliethoff, H.a}
}
