کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
761948 1462710 2014 17 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Discontinuous Galerkin and Petrov Galerkin methods for compressible viscous flows
ترجمه فارسی عنوان
روشهای متداول گالکرین و پتروف گالرکین برای جریانهای چسبندگی فشرده
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مکانیک محاسباتی
چکیده انگلیسی


• Discontinuous Galerkin and Petrov Galerkin methods are investigated and developed for laminar and turbulent flows.
• Curved surface mesh is generated using a CAPRI mesh parameterization tool for higher-order surface representations.
• Interior mesh is deformed via a linear elasticity strategy to obtain valid high-order finite element meshes.
• Accuracy is assessed between the discontinuous Galerkin and Petrov Galerkin discretization methods.

In this paper, high-order finite-element discretizations consisting of discontinuous Galerkin (DG) and streamline upwind/Petrov Galerkin (SUPG) methods are investigated and developed for solutions of two- and three-dimensional compressible viscous flows. Both approaches treat the discretized system fully implicitly to obtain steady state solutions or to drive unsteady problems at each time step. A modified Spalart and Allmaras (SA) turbulence model is implemented and is discretized to an order of accuracy consistent with the main Reynolds Averaged Navier–Stokes (RANS) equations using the present high-order finite-element methods. To accurately represent the real geometry configurations for viscous flows, high-order curved boundary meshes are generated via a Computational Analysis PRogramming Interface (CAPRI), while the interior meshes are deformed subsequently through a linear elasticity solver. The mesh movement procedure effectively avoids the generation of invalid elements that can occur due to the projection of curved physical boundaries and thus allows high-aspect-ratio curved elements in viscous boundary layers. Several numerical examples, including large-eddy simulations of viscous flow over a three-dimensional circular cylinder and turbulent flows over a NACA 4412 airfoil and a high-lift multi-element airfoil at high angles of attack, are considered to show the capability of the present high-order finite-element schemes in capturing typical viscous effects such as flow separation and to compare the accuracy between the high-order DG and SUPG discretization methods.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Computers & Fluids - Volume 100, 1 September 2014, Pages 13–29
نویسندگان
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