Design performance evaluation and vortex structure investigation of different S-shaped intermediate turbine ducts
Author:
Publisher
Springer Science and Business Media LLC
Subject
General Engineering,General Materials Science
Link
http://link.springer.com/content/pdf/10.1007/s11431-012-5041-0.pdf
Reference14 articles.
1. Miller R J, Moss R W, Ainsworth R W, et al. The development of turbine exit flow in aswan-necked inter-stage diffuser. ASME Paper GT2003-38174, 2003
2. Miller R J, Moss R W, Ainsworth R W, et al. The effect of an upstream turbine on a low-aspect ratio vane. ASME Paper, GT2004-54017, 2004
3. Marn A, Gottlich E, Pecnik R, et al. 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, GT2007-27405, 2007
4. Gottlich E, Marn A, Pecnik R, et al. 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, GT2007-28069, 2007
5. Axelsson L U, Johansson T G. Experimental investigation of the time-averaged flow in an intermediate turbine duct. ASME Paper, GT2008-50829, 2008
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