Implicit CFD methods for transitional shock wave – boundary layer interaction
نویسندگان
چکیده
منابع مشابه
Shock-boundary Layer Interaction (sbli) Cfd Research and Applications
Preamble Interaction of shock waves with turbulent boundary layers is important in many aerospace applications. Examples in external aerodynamics include control surfaces, wing body junctions, and multi-body aerodynamics. In high-speed propulsion systems, shock-boundary layer interaction (SBLI) can occur in intakes, supersonic combustion chambers and nozzles. Computational fluid dynamics (CFD) ...
متن کاملLow-frequency unsteadiness in shock wave–turbulent boundary layer interaction
Stephan Priebe and M. Pino Martín Journal of Fluid Mechanics / Volume 699 / May 2012, pp 1 49 DOI: 10.1017/jfm.2011.560, Published online: Link to this article: http://journals.cambridge.org/abstract_S002211201100560X How to cite this article: Stephan Priebe and M. Pino Martín (2012). Lowfrequency unsteadiness in shock wave–turbulent boundary layer interaction. Journal of Fluid Mechanics, 69...
متن کاملShock Wave / Boundary Layer Interaction Experiment on Control Surface
The shock wave / boundary layer interaction (SWBLI) experiment is part of the EXPERT mission. SWBLI is studied on two identical fixed compression ramps made of C/SiC, which are models for control surfaces. The flow separates on the flat surfaces upstream of the compression ramps and reattaches on the ramp surfaces. A reattachment shock results, which interacts with the boundary layer. One ramp ...
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The present work introduces a modified scheme for the solution of compressible 2-D full Navier-Stokes equations, using Flux Vector Splitting method. As a result of this modification, numerical diffusion is reduced. The computer code which is developed based on this algorithm can be used easily and accurately to analyze complex flow fields with discontinuity in properties, in cases such as shock...
متن کاملA Modified Flux Vector Splitting Scheme for Flow Analysis in Shock Wave Laminar Boundary Layer Interactions
The present work introduces a modified scheme for the solution of compressible 2-D full Navier-Stokes equations, using Flux Vector Splitting method. As a result of this modification, numerical diffusion is reduced. The computer code which is developed based on this algorithm can be used easily and accurately to analyze complex flow fields with discontinuity in properties, in cases such as shock...
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ژورنال
عنوان ژورنال: Aircraft Engineering and Aerospace Technology
سال: 2016
ISSN: 1748-8842
DOI: 10.1108/aeat-05-2015-0123