Transition Location Effect on Shock Wave Boundary Layer Interaction

Transition Location Effect on Shock Wave Boundary Layer Interaction

Experimental and Numerical Findings from the TFAST Project

Grothe, Patrick; Doerffer, Piotr; Petersen, Anna; Flaszynski, Pawel; Dussauge, Jean-Paul; Billard, Flavien; Babinsky, Holger

Springer Nature Switzerland AG

08/2021

540

Mole

Inglês

9783030474638

15 a 20 dias

831

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Introduction - TFAST Overview.- WP-1 Reference Cases of Laminar and Turbulent Interactions.- WP-2 Basic Investigation of Transition Effect.- WP-3 Internal Flows - Compressors.- WP-4 Internal Flows - Turbine.- WP-5 External Flows - Wing.- Closing Remarks.
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Laminar and Turbulent Boundary Layer;Shock Induced Separation;Transition Location Effect;Models of Flow Control Devices;Simulations of 3-D transonic Wing;Hybrid RANS-LENS Methods;URANS Methods;Reduce Flow Separation;Compressible Flows;Induced Transition to Turbulence;Transonic Turbine Flow;Transonic Wing Flow;Compressor and Fan Blade Aerodynamics;High Pressure Turbine Blade;TFAST Project;fluid- and aerodynamics