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USM3D (Legacy) References

  1. Frink, N. T., Pirzadeh, S. Z., Parikh, P., Pandya, M. J., and Bhat, M.,”The NASA Tetrahedral Unstructured Software System (TetrUSS),” To be presented at the 22nd Congress of the International Council of the Aeronautical Sciences (ICAS), Harrogate, UK, August 27-September 1, 2000.
  2. Frink, N. T.,”Three-Dimensional Upwind Scheme for Solving the Euler Equations on Unstructured Tetrahedral Grids,” Ph.D. Dissertation, Virginia Polytechnic Institute and State University, September 1991.
  3. Frink, N. T., “Upwind Scheme for Solving the Euler Equations on Unstructured Tetrahedral Meshes,”AIAA Journal, Vol. 30, No. 1, January 1992, pp. 70-77.
  4. Frink, N. T., “Recent Progress Towards a Three-Dimensional Unstructured Navier-Stokes Solver,” AIAA Paper 94-0061, January 1991.
  5. Frink, N. T.,”Tetrahedral Unstructured Navier-Stokes Method for Turbulent Flows,”AIAA Journal, Vol. 36, No. 11, November 1998, pp. 1975-1982.
  6. Bhat, M. K., and Parikh, P.,”Parallel Implementation of an Unstructured Grid-Based Navier-Stokes Solver,” AIAA Paper 99-0663, January 11-14, 1999.
  7. Karypis, G., and Kumar, V.,”Metis: A Software Package for Partitioning Unstructured Graphs, Partitioning Meshes, and computing Fill-Reducing Ordering of Sparse Matrices,” Version 3.0.3, University of Minnesota, November 1997.
  8. Pandya, M. J.,”Low Speed Preconditioning for an Unstructured Grid Navier-Stokes Solver, AIAA Paper 99-3134, June 28-July 1, 1999.
  9. Pandya, M. J., Bhat, M., and Parikh, P.,”Application of Unstructured Grid Methodology to Rotorcraft Flows,”Proceedings of the American Helicopter Society Rotorcraft Acoustics and Aerodynamics Specialists’ Meeting, Williamsburg, Virginia, October 28-30 1997.
  10. Pirzadeh, S.,”An Adaptive Unstructured Grid Method by Grid Subdivision, Local Remeshing, and Grid Movement,” AIAA Paper 99-3255, June 28-July 1, 1999.
  11. Cook, P., McDonald, M., and Firmin, M.,”Airfoil RAE 2822- Pressure Distributions and Boundary Layer Wake Measurement,” AR-138, AGARD Paper A6, 1979.
  12. Schmitt, V., and Charpin, F.,”Pressure Distributions on the ONERA-M6 Wing at Transonic Mach Number,” AGARD AR 138, May 1979.
  13. Cavallo, P. A.,”Coupling Static Aeroelastic Predictions with an Unstructured Grid Euler/Interacting Boundary Layer Method,” Masters Thesis, The George Washington University, July 1995.
  14. Parikh, P.,”Development of a Modular Aerodynamic Design System based on Unstructured Grids,” AIAA Paper 97-0172.
  15. Jacobs, P. F.,”Experimental Trim Drag Values and Flow Field Measurements for a Wide-Body Transport Model with a Conventional and Supercritical Wings,” NASA TP 2071, 1982.