A combustor liner cooling system design methodology based on a fluid/structure approach

Author:

Laraia Massimo,Manna Marcello,Cinque Giuseppe,Di Martino Pasquale

Funder

European Commission

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Energy Engineering and Power Technology

Reference90 articles.

1. Gas Turbine Combustion;Lefebvre,1983

2. R.J. Goldstein, D.E. Metzger, A.I. Leont'ev, Heat transfer in turbomachinery, in: Proc. of the Int. Symposium on Heat Transfer in Turbomachinery, Greece, 1992.

3. Experimental and numerical study of heat transfer in a gas turbine combustor liner;Bailey;J. Eng. Gas Turbines Power,2003

4. Geometric and aero-thermal influences on multiholed plane temperature: application on combustor wall;Leger;Int. J. Heat Mass Transf.,2003

5. Combustion and cooling performance in an aero-engine annular combustor;Li;Appl. Therm. Eng.,2006

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