Transition Location Effect on Shock Wave Boundary Layer Interaction Piotr Doerff
Titel: Transition Location Effect on Shock Wave Boundary Layer Interaction, Untertitel: Experimental and Numerical Findings from the TFAST Project, Einband: Taschenbuch, Autor: Piotr Doerffer, Verlag: Springer International Publishing, Springer International Publishing, Sprache: Englisch, Seiten: 548, Maße: 235x155x30 mm, Gewicht: 820 g, Verkäufer: buch-mimpf, Schlagworte: Compressible flows Compressor and Fan Blade Aerodynamics High Pressure Turbine Blade Hybrid RANS-LENS Methods Induced Transition to Turbulence Laminar and Turbulent Boundary Layer Models of Flow Control Devices Reduce Flow Separation Shock Induced Separation Simulations of 3-D transonic Wing TFAST Project Transition Location Effect Transonic Turbine Flow Transonic Wing Flow URANS Methods fluid- and aerodynamics.
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