High-order strand grid methods for shock turbulence interaction
Author:
Affiliation:
1. Department of Mechanical and Aerospace Engineering, Utah State University, Logan, UT, USA
2. Department of Mechanical Engineering, Stanford University, Stanford, CA, USA
Funder
U.S. Department of Defense HPC Modernisation Program Office
Office of Naval Research Sea-Based Aviation program
Publisher
Informa UK Limited
Subject
Mechanical Engineering,Mechanics of Materials,Energy Engineering and Power Technology,Condensed Matter Physics,Aerospace Engineering,Computational Mechanics
Link
https://www.tandfonline.com/doi/pdf/10.1080/10618562.2018.1490411
Reference28 articles.
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3. A simple robust and accurate a posteriori sub-cell finite volume limiter for the discontinuous Galerkin method on unstructured meshes
4. Hemisphere-cylinder in transonic flow, free-stream Mach number from 0.7 to 1.0
5. ANALYSIS AND DESIGN OF NUMERICAL SCHEMES FOR GAS DYNAMICS, 1: ARTIFICIAL DIFFUSION, UPWIND BIASING, LIMITERS AND THEIR EFFECT ON ACCURACY AND MULTIGRID CONVERGENCE
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