Transition Location Effect on Shock Wave Boundary Layer Interaction
portes grátis
Transition Location Effect on Shock Wave Boundary Layer Interaction
Experimental and Numerical Findings from the TFAST Project
Doerffer, Piotr; Petersen, Anna; Grothe, Patrick; Flaszynski, Pawel; Babinsky, Holger; Billard, Flavien; Dussauge, Jean-Paul
Springer Nature Switzerland AG
08/2021
540
Mole
Inglês
9783030474638
15 a 20 dias
831
Descrição não disponível.
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.
Este título pertence ao(s) assunto(s) indicados(s). Para ver outros títulos clique no assunto desejado.
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
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.
Este título pertence ao(s) assunto(s) indicados(s). Para ver outros títulos clique no assunto desejado.
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
