Modelling strategies for the prediction of hot streak generation in lean burn aeroengine combustors

Author:

Andreini AntonioORCID,Bacci TommasoORCID,Insinna MassimilianoORCID,Mazzei LorenzoORCID,Salvadori Simone

Funder

European Commission

MIUR

CINECA award

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference51 articles.

1. Developments in hot-streak simulators for turbine testing;Povey;ASME J. Turbomach.,2009

2. Effects of combustor exit profiles on vane aerodynamic loading and heat transfer in a high pressure turbine;Barringer;ASME J. Turbomach.,2009

3. Aerodynamics and heat transfer for a cooled one and one-half stage high-pressure turbine, part iii: impact of hot-streak characteristics on blade row heat flux;Mathison;ASME J. Turbomach.,2012

4. The effect of hot-streaks on hp vane surface and endwall heat transfer: an experimental and numerical study;Povey;ASME J. Turbomach.,2007

5. A hot-streak (combustor) simulator suited to aerodynamic performance measurements;Povey;Proc. Inst. Mech. Eng., G J. Aerosp. Eng.,2008

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