Reacting Gas Adjoint-Based Grid Adaptation in FUN3D

Author:

Basore Kevin1

Affiliation:

1. Universities Space Research Association

Publisher

American Institute of Aeronautics and Astronautics

Reference6 articles.

1. Unstructured Grid Adaptation: Status, Potential Impacts, and Recommended Investments Towards CFD 2030

2. Park, M. A. “Anisotropic Output-Based Adaptation with Tetrahedral Cut Cells for Compressible Flows,” Ph.D. thesis,Massachusetts Institute of Technology, 2008.

3. Biedron, R. T., Carlson, J.R., Derlaga, J. M., Gnoffo, P. A., Hammond, D. P., Jones, W. T., Kleb, B., Lee-rausch, E. M. Nielsen, E. J., Park, M. A., Rumsey, C. L., Thomas, J. L., and Wood, W. A. “FUN3D Manual: 13.1,” Tech. Rep. February, National Aeronautics and Space Administration, 2017.

4. Thompson, K. B. “Aerothermodynamic Design Sensitivities for a Reacting Gas Flow Solver on an Unstructured Mesh Using a Discrete Adjoint Formulation,” Ph.D. thesis,North Carolina State University, 2017.

5. Parallel, Gradient-Based Anisotropic Mesh Adaptation for Re-Entry Vehicle Configuratons

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