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Dive into the research topics where Ryan S. Glasby is active.

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Featured researches published by Ryan S. Glasby.


54th AIAA Aerospace Sciences Meeting | 2016

Introduction to COFFE: The Next-Generation HPCMP CREATE-AV CFD Solver

Ryan S. Glasby; J. Taylor Erwin; Douglas L. Stefanski; Steven R. Allmaras; Marshall C. Galbraith; W. Kyle Anderson; Robert H. Nichols

HPCMP CREATE-AV Conservative Field Finite Element (COFFE) is a modular, extensible, robust numerical solver for the Navier-Stokes equations that invokes modularity and extensibility from its first principles. COFFE implores a flexible, class-based hierarchy that provides a modular approach consisting of discretization, physics, parallelization, and linear algebra components. These components are developed with modern software engineering principles to ensure ease of uptake from a users or developers perspective. The Streamwise Upwind/Petrov-Galerkin (SU/PG) method is utilized to discretize the compressible Reynolds-Averaged Navier-Stokes (RANS) equations tightly coupled with a variety of turbulence models. The mathematics and the philosophy of the methodology that makes up COFFE are presented.


51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition | 2013

Comparison of SU/PG and DG Finite-Element Techniques for the Compressible Navier-Stokes Equations on Anisotropic Unstructured Meshes

Ryan S. Glasby; Arnold Afb; Nicholas K. Burgess; W. Kyle Anderson; Li Wang; Dimitri J. Mavriplis; Steven R. Allmaras

In this paper computed results from Steamline Upwind/Petrov-Galerkin and Discontinuous Galerkin finite-element methods are compared for various two-dimensional compressible Navier-Stokes applications. Identical meshes are utilized for each comparison with linear, quadratic, and cubic elements employed. The order of accuracy is assessed for each scheme for viscous flows using the method of manufactured solutions, and results from each scheme are compared to experimental data. Each scheme is notionally of design order, and results from both compare well with experimental data. Both schemes are viable finite-element discretization techniques, and neither applies an unnecessary amount of artificial dissipation.


46th AIAA Fluid Dynamics Conference | 2016

High-Order Mesh Curving Using WCN Mesh Optimization

Steve L. Karman; Jon T. Erwin; Ryan S. Glasby; Douglas L. Stefanski


55th AIAA Aerospace Sciences Meeting | 2017

Results from HPCMP CREATETM-AV Kestrel Component COFFE for the 6th Drag Prediction Workshop Cases

Jon T. Erwin; Ryan S. Glasby; Douglas L. Stefanski; Steve L. Karman


54th AIAA Aerospace Sciences Meeting | 2016

Application of HPCMP CREATETM-AV COFFE for Three-Dimensional Turbulent Flow Cases

Jon T. Erwin; Ryan S. Glasby


2018 AIAA Aerospace Sciences Meeting | 2018

High-Order Time-Accurate Simulations using HPCMP CREATE(TM)-AV Kestrel Component COFFE

Kevin R. Holst; Ryan S. Glasby; Jon T. Erwin; Douglas L. Stefanski; Ryan B. Bond


2018 AIAA Aerospace Sciences Meeting | 2018

High-Order Large Eddy Simulation Validation in HPCMP CREATE(TM)-AV Kestrel Component COFFE

Kevin R. Holst; Ryan S. Glasby; Jon T. Erwin; Douglas L. Stefanski; Ryan B. Bond


Journal of Aircraft | 2017

Comparison of Fixed and Adaptive Unstructured Grid Results for Drag Prediction Workshop 6

Todd R. Michal; Deric Babcock; Dmitry S. Kamenetskiy; Joshua Krakos; Mortaza Mani; Ryan S. Glasby; Taylor Erwin; Douglas L. Stefanski


55th AIAA Aerospace Sciences Meeting | 2017

Results from HPCMP CREATETM-AV Kestrel Components KCFD and COFFE for the Open Source Fighter

David Hine; Ryan S. Glasby; Jon T. Erwin; Douglas L. Stefanski


55th AIAA Aerospace Sciences Meeting | 2017

Finite-element solutions to the Reynolds Averaged Navier-Stokes equations using a Spalart-Allmaras Turbulence Model

Nicholas K. Burgess; Ryan S. Glasby; Jon T. Erwin; Douglas L. Stefanski; Steven R. Allmaras

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Jon T. Erwin

University of Tennessee

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Ryan B. Bond

University of Tennessee

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Steven R. Allmaras

Massachusetts Institute of Technology

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W. Kyle Anderson

University of Tennessee at Chattanooga

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