Influence of Reynolds Number on the Unsteady Aerodynamics of Integrated Aggressive Intermediate Turbine Duct

Author:

Liu Hongrui,Liu Jun,Ji Lucheng,Du Qiang,Liu Guang,Wang Pei

Publisher

Springer Science and Business Media LLC

Subject

Condensed Matter Physics

Reference21 articles.

1. Miller R.J., Moss R.W., Ainsworth R.W., Harvey N.W.. The development of turbine exit flow in a Swan-Necked Inter-Stage diffuser. Proceedings of ASME Turbo Expo 2003, Georgia, USA, GT2003-38174.

2. Axelsson L.-U., Johansson T.G.. Evaluation of the flow in an intermediate turbine duct at Off-Design conditions, 26th International Congress of The Aeronautical Sciences, Anchorage, Alaska, USA, 2008.

3. Axelsson L.-U., George W.K.. Spectral analysis of the flow in an intermediate turbine duct. Proceedings of ASME Turbo Expo 2008, Berlin, Germany, GT2008-51340.

4. Wallin F., Osso C.A., Johansson T.G. Experimental and numerical investigation of an aggressive intermediate turbine duct: Part 1–Flowfield at Design Inlet Conditions. 26th AIAA Applied Aerodynamics Conference, Honolulu, Hawaii, 2008, AIAA 2008–7055.

5. Osso C.A., Wallin F., Johansson T.G.. Experimental and numerical investigation of an aggressive intermediate turbine duct–Part 2: flowfield under Off-Design inlet conditions. 26th AIAA Applied Aerodynamics Conference, Honolulu, Hawaii, 2008, AIAA 2008–7056.

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