Experimental Heat Transfer Investigation of an Aggressive Intermediate Turbine Duct
Author:
Affiliation:
1. Volvo Aero Corporation,Trollhättan, Sweden; Chalmers University of Technology, Göteborg, Sweden
2. Chalmers University of Technology, Göteborg, Sweden
3. Volvo Aero Corporation, Trollhättan, Sweden
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4004779/5850965/051026_1.pdf
Reference17 articles.
1. Dominy, R. G., Kirkham, D. A., and Smith, A. D., 1996, “Flow Development Through Inter-Turbine Diffusers,” ASME Paper No. 96-GT-139.
2. Miller, R. J., Moss, R. W., Ainsworth, R. W., and Harvey, N. W., 2004, “The Effect of an Upstream Turbine on a Low-Aspect Ratio Vane,” ASME Paper No. GT2004-54017.
3. Experimental Investigation of the Flow Through an Aggressive Intermediate Turbine Duct Downstream of a Transonic Turbine Stage;Göttlich
4. Marn, A., Göttlich, E., Pecnik, R., Malzacher, F. J., Schennach, O., and Pirker, H. P., 2007, “The Influence of Blade Tip Gap Variation on the Flow Through an Aggressive S-shaped Intermediate Turbine Duct Downstream a Transonic Turbine Stage—Part I: Time-averaged Results,” ASME Paper No. GT2007-27405.
5. Göttlich, E., Marn, A., Pecnik, R., Malzacher, F. J., Schennach, O., and PirkerH. P., 2007, “The Influence of Blade Tip Gap Variation on the Flow Through an Aggressive S-shaped Intermediate Turbine Duct Downstream a Transonic Turbine Stage—Part II: Time-resolved Results and Surface Flow,” ASME Paper No. GT2007-28069.
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