A Compressible Pressure-based Solution Algorithm for Gas Turbine Combustion Chambers Using the PDF/FGM Model

Author:

Klapdor E. V.,di Mare F.,Kollmann W.,Janicka J.

Publisher

Springer Science and Business Media LLC

Subject

Physical and Theoretical Chemistry,General Physics and Astronomy,General Chemical Engineering

Reference47 articles.

1. An, B.-T., Liu, J.-J., Jiang, H.-D.: Combined unsteady effects of hot streak and trailing edge coolant ejection in a turbine stage. In: Proceedings of ASME TurboExpo 2009, Orlando, FL. ASME Paper GT2009-59473 (2009)

2. An, B.-T., Liu, J.-J., Jiang, H.-D.: Numerical investigation on unsteady effects of hot streak on flow and heat transfer in a turbine stage. ASME J. Turbomach. 131, 031015-1-15 (2009)

3. Barlow, R., Frank, J.: Piloted CH4/Air Flames C, D, E and F—Release 2.1. http://www.ca.sandia.gov/TNF (2007)

4. Barringer, M.D., Thole, K.A., Polanka, M.D., Clark, J.P., Koch, P.J.: Migration of combustor exit profiles through high pressure turbine vanes. ASME J. Turbomach. 131, 021010-1-10 (2009)

5. Bastiaans, R.J.M., Vreman, A.W., Pitsch, H.: DNS of Lean Hydrogen Combustion with Flamelet-generated Manifolds. Center for Turbulence Research, Annual Research Briefs, Stanford (2007)

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