Introduction to Unsteady Shock Shock And Shock Boundary Layer Interactions
Exploring Unsteady Shock Shock And Shock Boundary Layer Interactions reveals several interesting facts. Detailed information: Physics of Fluids 28, 096101 (2016) http://dx.doi.org/10.1063/1.4961571.
Unsteady Shock Shock And Shock Boundary Layer Interactions Comprehensive Overview
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Mach 2.85 over 20 degrees wedge. SST k-Omega.
Summary & Highlights for Unsteady Shock Shock And Shock Boundary Layer Interactions
- Shock
- D'Alembert's Paradox, Prandtl
- Wind tunnel Mach numer 2.0
- Lennart Rohlfs, Julien Weiss, Chair of Aerodynamics, TU Berlin: Flow Physics of a Turbulent Shockwave/
- Luis Laguarda Sanchez.
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