Numerical Investigation on the Effects of Cavity-Blowing Jet on Intermediate Turbine Duct Flowfield

Author:

Liu JunORCID,Du Qiang

Funder

NSFC

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering

Reference25 articles.

1. Johansson PBV, Axelsson L-U (2009) numerical and experimental analysis of the flow in an aggressive intermediate turbine duct. In: Proceedings of ASME turbo expo. Paper-No. GT2009-59299

2. Marn A, Göttlich E, Pecnik R, Malzacher FJ, Schennach O, Pirker HP (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. In: Proceedings of ASME turbo expo. Paper-No. GT2007-27405

3. Marn A, Göttlich E, Malzacher F, Pirker HP (2009) The effect of rotor tip clearance size onto the separation flow though a super-aggressive S-shaped intermediate turbine duct downstream of a transonic turbine stage. In: Proceedings of ASME Turbo Expo. Paper-No. GT2009-59934

4. Göttlich E, Marn A, Pecnik R, Malzacher FJ, Schennach O, Pirker HP (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. In: Proceedings of ASME Turbo Expo GT2007-28069

5. Sanz W, Kelterer M, Pecnik R, Marn A, Göttlich E (2009) Numerical investigation of the effect of tip leakage flow on an aggressive S-shaped intermediate turbine duct. In: Proceedings of ASME turbo expo. Paper-No. GT2009-59535

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