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USM3D-ME References

Code Development and Verification

  1. Pandya, M. J., Frink, N. T., Ding, E., and Parlette, E. B., “Toward Verification of USM3D Extensions for Mixed Element Grids,” AIAA Paper 2013-2541, 31st Applied Aerodynamics Conference, San Diego, CA, June 2013; DOI: 10.2514/6.2013-2541
  2. Pandya, M. J., Diskin B., Thomas, J. L., and Frink N. T., “Improved Convergence and Robustness of USM3D Solutions on Mixed Element Grids,” AIAA Journal (2016), 54(9), pp. 2589-2610; DOI: 10.2514/1.J054545
  3. Pandya, M. J., Diskin B., Thomas, J. L., and Frink N. T., “Assessment of USM3D Hierarchical Adaptive Nonlinear Method Preconditioners for Three-Dimensional Cases,” AIAA Journal (2017) 55(10), pp. 3409-3424; DOI:10.2514/1.J055823
  4. Pandya, M. J., Jespersen, D. C., Diskin B., Thomas, J. L., and Frink, N. T., “Efficiency of Mixed-Element USM3D for Benchmark Three-Dimensional Flows,” AIAA Journal (2021), 59(8), pp. 2997-3011; DOI: 10.2514/1.J059720
  5. Pandya M. J., Jespersen, D. C., Diskin B., Thomas, J. L., and Frink, N. T., “Verification and Scalability of Mixed-Element USM3D for Benchmark Three-Dimensional Flows,” AIAA Journal (2021), 59(11), pp. 4719-4738; DOI: 10.2514/1.J060064
  6. Elmiligui, A., Pandya, M.J., Carter, M., Diskin, B., and Nayani, S., “USM3D Simulations for the Third AIAA Sonic Boom Prediction Workshop,” Journal of Aircraft (2022), 59(3), pp. 647–659; DOI: 10.2514/1.C036429
  7. Pandya, M. J., Diskin B., Thomas, J. L., and Frink, N. T., “Improved Convergence and Robustness of USM3D Solutions on Mixed Element Grids,” AIAA-2015-1747, SciTech-2015, Kissimmee, Florida, FL, January 2015; DOI: 10.2514/6.2015-1747
  8. Pandya, M. J., Diskin, B., Thomas, J. L., and Frink, N. T., “Assessment of Preconditioner for a USM3D Hierarchical Adaptive Nonlinear Iteration Method (HANIM),” AIAA-2016-0860, SciTech-2016, San Diego, CA, January 2016; DOI: 10.2514/6.2016-0860
  9. Pandya, M. J., Jespersen, D. C., Diskin B., Thomas, J. L., and Frink, N. T., “Accuracy, Scalability, and Efficiency of Mixed-Element USM3D for Benchmark Three-Dimensional Flows,” AIAA-2019-2333, SciTech-2019, San Diego, CA, January 2019; DOI: 10.2514/6.2019-2333
  10. Elmiligui, A., Pandya, M.J., Carter, M., Diskin, B., and Nayani, S., “USM3D Simulations for the Third AIAA Sonic Boom Prediction Workshop,” AIAA-2021-0470, SciTech-2021, Virtual Event, January 2021; DOI: 10.2514/6.2021-0470
  11. Diskin, B., Pandya, M. J., Pomeroy, B. W., and Boyett, T., “USM3D-ME Revised SA-neg Implementation and Assessment for Seventh Drag Prediction Workshop Solutions,” AIAA 2023-3252, Aviation-2023, San Diego, CA, June 2023; DOI: 10.2514/6.2023-3252

Verification Studies and Applications

  1. Diskin B., Thomas, J.L., Rumsey, C.L., and Pandya, M.J., “Reference Solutions for Benchmark Three Dimensional Turbulent Flows,” AIAA-2016-0858, SciTech-2016, San Diego, CA, January 2016; DOI: 10.2514/6.2016-0858
  2. Diskin B., Anderson, W.K., Pandya, M.J., Rumsey, C.L., Lui, Y., and Nishikawa H., “Grid Convergence of Three-Dimensional Benchmark Turbulent Flows,” AIAA-2018-1102, SciTech-2018, Kissimmee, FL, January 2018; DOI: 10.2514/6.2018-1102
  3. Frink, N.T., Hiller, B.R., Murphy, P.C., Cunningham, K., and Shah, G.H., “Investigation of Reduced-Order Modeling for Aircraft Stability and Control Prediction,” AIAA Paper 2019-0980; DOI: 10.2514/6.2019-0980
  4. Diskin, B., Ahmad, N.N., Anderson, W.K., Derlaga, J.M., Pandya, M.J., Rumsey, C.L., Wang, L., Wood, S.L., Liu, Y., Nishikawa, H., and Galbraith, M., “Verification Test Suite for Spalart-Allmaras QCR2000 Turbulence Model,” AIAA 2021-1552.c1, SciTech-2021, Virtual Event, January 2021; DOI: 10.2514/6.2021-1552.c1
  5. Bozeman, M.D., Pandya, M.J., and Park, M.A., “Mixed-Element USM3D Contributions to the 4th AIAA High-Lift Prediction Workshop,” AIAA-2023-1759, SciTech-2023, National Harbor, MD, January 2023; DOI: 10.2514/6.2023-1759