Output-Based Adaptive RANS Solutions using Higher-Order FEM on a Multi-Element Airfoil

Ursachi, Carmen-Ioana; Galbraith, Marshall C.; Allmaras, Steven R.; Darmofal, David L.

doi:10.2514/6.2020-3220

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Cited by 6 publications

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A Perspective on the State of Aerospace Computational Fluid Dynamics Technology

Mani

Dorgan

2023

Annu. Rev. Fluid Mech.

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Over the past several decades, computational fluid dynamics has been increasingly used in the aerospace industry for the design and study of new and derivative aircraft. In this review we survey the CFD application process and note its place and importance within the everyday work of industry. Furthermore, the centrality of geometry and importance of turbulence models, higher-order numerical algorithms, output-based mesh adaptation, and numerical design optimization are discussed. Challenges in each area are noted and specific suggestions for investment are made. The review concludes with an outlook toward a future in which certification by analysis and model-based design are standard practice, along with a reminder of the steps necessary to lead the industry there.

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A Perspective on the State of Aerospace Computational Fluid Dynamics Technology

Mani

Dorgan

2023

Annu. Rev. Fluid Mech.

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show abstract

A Robust Monolithic Nonlinear Newton Method for the Compressible Reynolds Averaged Navier-Stokes Equations

SAHIN,

Sukas

2024

Preprint

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Comparisons of HPCMP CREATE^TM-AV Kestrel-COFFE, SU2, and MIT SANS RANS Solutions using Output-Based Adapted Meshes for a Multi-Element Airfoil

Galbraith

Ursachi

Chandel

et al. 2021

AIAA Scitech 2021 Forum

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Output-Based Adaptive RANS Solutions using Higher-Order FEM on a Multi-Element Airfoil

Cited by 6 publications

References 18 publications

A Perspective on the State of Aerospace Computational Fluid Dynamics Technology

A Perspective on the State of Aerospace Computational Fluid Dynamics Technology

A Robust Monolithic Nonlinear Newton Method for the Compressible Reynolds Averaged Navier-Stokes Equations

Comparisons of HPCMP CREATE^TM-AV Kestrel-COFFE, SU2, and MIT SANS RANS Solutions using Output-Based Adapted Meshes for a Multi-Element Airfoil

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Output-Based Adaptive RANS Solutions using Higher-Order FEM on a Multi-Element Airfoil

Cited by 6 publications

References 18 publications

A Perspective on the State of Aerospace Computational Fluid Dynamics Technology

A Perspective on the State of Aerospace Computational Fluid Dynamics Technology

A Robust Monolithic Nonlinear Newton Method for the Compressible Reynolds Averaged Navier-Stokes Equations

Comparisons of HPCMP CREATETM-AV Kestrel-COFFE, SU2, and MIT SANS RANS Solutions using Output-Based Adapted Meshes for a Multi-Element Airfoil

Contact Info

Product

Resources

About

Comparisons of HPCMP CREATE^TM-AV Kestrel-COFFE, SU2, and MIT SANS RANS Solutions using Output-Based Adapted Meshes for a Multi-Element Airfoil