Heat transfer research on gas turbine airfoils at NASA GRC

Author:

Garg Vijay K.

Publisher

Elsevier BV

Subject

Fluid Flow and Transfer Processes,Mechanical Engineering,Condensed Matter Physics

Reference77 articles.

1. Transition modeling effects on turbine rotor blade heat transfer predictions;Ameri;J. Turbomachinery,1996

2. Heat transfer and flow on the first-stage blade tip of a power generation gas turbine: part 2 – simulation results;Ameri;J. Turbomachinery,2000

3. Ameri, A.A., Rigby, D.L., 1999. A numerical analysis of heat transfer and effectiveness on film cooled turbine blade tip models. NASA CR 1999-209165. Also Proc. 14th Internat. Symp. Air Breathing Engines (ISABE), Florence, Italy

4. Ameri, A.A., Steinthorsson, E., 1995. Prediction of unshrouded rotor blade tip heat transfer. ASME Paper 95-GT-142

5. Ameri, A.A., Steinthorsson, E., 1996. Analysis of gas turbine rotor blade tip and shroud heat transfer. ASME Paper 96-GT-189

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