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3-D Nozzle project Project supervisor T.H. Fransson Students O. Bron, A. Kessar

Background: Large influence of unsteady flow effects in turbomachinery flow Strong interactions between Steady and Unsteady Flows influence on shock motion influence separation influence on far acoustic field. 3-D Nozzle project Project supervisor T.H. Fransson Students O. Bron, A. Kessar.

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3-D Nozzle project Project supervisor T.H. Fransson Students O. Bron, A. Kessar

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  1. Background: Large influence of unsteady flow effects in turbomachinery flow Strong interactions between Steady and Unsteady Flows influence on shock motion influence separation influence on far acoustic field 3-D Nozzle projectProject supervisorT.H. FranssonStudentsO. Bron, A. Kessar Engine Compressor Stage • Objectives: Establish a better understanding of fundamental steady/unsteady flow interactions by analysing: • Unsteady shock motion • Separated zone motion • Importance of the “acoustic blockage” in 2D transonic flow • Non-linear shock/boundary layer interaction in unsteady flows at different operating conditions Interblade Passage 1\3

  2. e 3-D Nozzle project: Experimental part • Facility: • Test objects (2-D\3-D bumps), simulating interblade passage. • Unsteadiness introduced by back pressure fluctuations generator. Picture of the Test section • Measurement Techniques: • Oil & conventional Schlieren visualisations, Hotfilm/Hotwire measurements, surfacepressure maping (both steady-state and high frequency), LDA & 3D-L2F velocity measurements, PIV... Schlieren visualisation 2\3

  3. 3-D Nozzle project: Numerical part • Simulations: • 2D/3D steady/unsteady RANS • with k- turbulent model • Simulations of both 2-D/3-D test objects • Interaction phenomena modelisation • Exp-Num Comparison: • Qualitative & quantitative comparison • Validation of physical/numerical models • Database elaboration 50% channel 3\3

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