High-order discontinuous Galerkin RANS solutions of the incompressible flow over a delta wing

Author:

Crivellini Andrea,D’Alessandro Valerio,Bassi Francesco

Publisher

Elsevier BV

Subject

General Engineering,General Computer Science

Reference41 articles.

1. The second international vortex flow experiment (VFE-2);Hummel;Notes Numer Fluid Mech Multidiscip Des,2009

2. Furman A, Breitsamter C. ICAS 2006, investigation of flow phenomena on generic delta wing. In: 25th International congress of the aeronautical sciences. Hamburg, Germany: German Society for Aeronautics and Astronautics (DGLR), September 3–8 2006.

3. Furman A, Breitsamter C. Turbulent and unsteady flow charachteristics of delta wing vortex systems. In: 46th AIAA aerospace sciences meeting and exhibit. Reno (NV), United States: AIAA, January 7–10 2008.

4. Furman A, Breitsamter C. Experimental investigations on the VFE-2 configuration at TU Munich, Germany. Understanding and modeling vortical flows to improve the technology readiness level for military aircraft. Technical Report RTO-TR-AVT-113, RTO/NATO, Neuilly-sur-Seine Cedex, Cedex, October 2009.

5. Turbulent and unsteady flow characteristics of delta wing vortex systems;Furman;Aerosp Sci Technol,2013

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2. A quadrature simplification method for fast implicit discontinuous Galerkin schemes;Computers & Fluids;2018-05

3. Wall Modeled Large Eddy Simulation of the VFE-2 Delta Wing;Direct and Large-Eddy Simulation X;2017-10-08

4. Wall Modeled Large Eddy Simulation of a Delta Wing with Round Leading Edge;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2016

5. Wall modeled large eddy simulation of the VFE-2 delta wing;33rd AIAA Applied Aerodynamics Conference;2015-06-19

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