High-Order Methods for Large-Eddy Simulation in Complex Geometries

2009 ◽  
pp. 309-334
Author(s):  
Christine Baur ◽  
Patrick Bontoux ◽  
Michael Kornhaas ◽  
Mathieu Minguez ◽  
Richard Pasquetti ◽  
...  
Keyword(s):  
Large Eddy Simulation ◽  
High Order ◽  
Complex Geometries ◽  
High Order Methods ◽  
Eddy Simulation ◽  
Large Eddy

Large Eddy Simulation of Single Stream Jet Using High-Order Methods

2021 ◽  
pp. 407-432
Author(s):  
J. F. Boussuge ◽  
R. Biolchini ◽  
M. Lorteau ◽  
M. de la Llave Plata ◽  
N. Lupoglazoff ◽  
...  
Keyword(s):  
Large Eddy Simulation ◽  
High Order ◽  
High Order Methods ◽  
Eddy Simulation ◽  
Single Stream ◽  
Large Eddy

Towards High-Order Large Eddy Simulation of Aero-Thermal Flows for Turbomachinery Applications

2017 ◽  
Author(s):  
R. Bhaskaran ◽  
Feilin Jia ◽  
Gregory M. Laskowski ◽  
Z. J. Wang ◽  
Umesh Paliath
Keyword(s):  
Heat Transfer ◽  
Large Eddy Simulation ◽  
Numerical Algorithms ◽  
High Order ◽  
Sixth Order ◽  
Computational Grids ◽  
Variable Order ◽  
Free Stream Turbulence ◽  
Eddy Simulation ◽  
Large Eddy

The solution accuracy and computational efficiency of high order Large Eddy Simulation (LES) solvers are evaluated on two benchmark open literature blade cascade problems. The first problem concerns wake development in the T106A low pressure turbine cascade [1]. The second problem examines the effect of free-stream turbulence on heat transfer from the VKI first stage high pressure turbine vane [2]. The calculations are performed with two independently developed high order LES solvers using completely different numerical algorithms. The first solver FDL3Di [3] was originally developed at the Airforce Research Laboratory (AFRL) and employs structured overset grids. It uses a sixth order compact finite difference scheme in space along with an implicit Beam-Warming scheme for time marching. The second solver, hpMusic, is developed at the University of Kansas [4]. This is a variable order (up to sixth order) unstructured grid solver employing a discontinuous formulation known as flux reconstruction (FR) / correction procedure via reconstruction (CPR) [5]. The computational grids used are independently tuned for each application. The solvers are benchmarked against experimental data for wake development and blade heat transfer coefficient. Further physical insights in to the test cases are also obtained, filling gaps in experimental results, especially for the VKI problem.

scholarly journals Evaluation of Second- and High-Order Solvers in Wall-Resolved Large-Eddy Simulation

AIAA Journal ◽  
2019 ◽  
Vol 57 (4) ◽  
pp. 1636-1648 ◽  
Author(s):  
Feilin Jia ◽  
Jeremy Ims ◽  
Z. J. Wang ◽  
James Kopriva ◽  
Gregory M. Laskowski
Keyword(s):  
Large Eddy Simulation ◽  
High Order ◽  
Eddy Simulation ◽  
Large Eddy
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