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If you are using SU2 in your research, please cite and support our work. If you would like to contribute to the development of the SU2 suite, please contact the developers. Thanks!

 

F. Palacios, M. R. Colonno, A. C. Aranake, A. Campos, S. R. Copeland, T. D. Economon, A. K. Lonkar, T. W. Lukaczyk, T. W. R. Taylor, and J. J. Alonso, “Stanford University Unstructured (SU2): An open-source integrated computational environment for multi-physics simulation and design”, AIAA Paper 2013-0287, 51st AIAA Aerospace Sciences Meeting and Exhibit. January 7th - 10th, 2013. Grapevine, Texas, USA.

SU2 is being used actively in the research community to perform cutting edge analysis and design.  The following technical publications have cited the suite:

  • Palacios, F., Alonso, J. J., Colonno, M., Hicken, J., and Lukaczyk, T., "Adjoint-based Method for Supersonic Aircraft Design Using Equivalent Area Distributions," 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, AIAA Paper 2012-0269, Nashville, TN, January 2012.
  • Economon, T. D., Palacios, F., Alonso, J. J., "Optimal Shape Design for Open Rotor Blades," 30th AIAA Applied Aerodynamics Conference, AIAA Paper 2012-3018, New Orleans, LA, June 2012.
  • Palacios, F., Jameson, A., Alonso, J. J., "Shape Sensitivity of Free-Surface Interfaces Using a Level Set Methodology," 30th AIAA Applied Aerodynamics Conference, AIAA Paper 2012-3341, New Orleans, LA, June 2012.
  • Lonkar, A., Palacios, F., MacCormack, R., A., Alonso, J. J., "Multidimensional Simulation of Plasma in Argon through a Shock in Hypersonic Flow," 30th AIAA Applied Aerodynamics Conference, AIAA Paper 2012-3105, New Orleans, LA, June 2012.
  • Taylor, T., Palacios, F., Duraisamy, K., A., Alonso, J. J., "Towards a Hybrid Adjoint Approach for Arbitrarily Complex Partial Differential Equations," 30th AIAA Applied Aerodynamics Conference, AIAA Paper 2012-3342, New Orleans, LA, June 2012.
  • Lukaczyk, T., Colonno, M., Palacios, F., and Alonso, J. J., "Response Surface Methodologies for Low-Boom Supersonic Aircraft Design using Equivalent Area Distributions," 12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, AIAA Paper 2012-5707, Indianapolis, IN, September 2012.
  • Economon, T. D., Palacios, F., Alonso, J. J., "A Coupled-Adjoint Method for Aerodynamic and Aeroacoustic Optimization," 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, AIAA Paper 2012-5598, Indianapolis, IN, Sept. 2012.
  • Colonno, M., Naik, K., Duraisamy, K., Alonso, J. J., "An Adjoint-Based Multidisciplinary Optimization Framework for Rotorcraft Systems," 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, AIAA Paper 2012-5656, Indianapolis, IN, Sept. 2012.
  • Palacios, F., Colonno, M. R., Aranake, A. C., Campos, A., Copeland, S. R., Economon, T. D., Lonkar, A. K., Lukaczyk,T. W., Taylor, T. W. R., and Alonso, J. J., “Stanford University Unstructured (SU2): An open-source integrated computational environment for multi-physics simulation and design,” 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, AIAA Paper 2013-0287, Grapevine, TX, Jan. 2013.
  • Aranake, A., Lakshminarayan, V., Duraisamy, K., "Computational Analysis of Shrouded Wind Turbine Configurations," 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, AIAA Paper 2013-1211, Grapevine, TX, Jan. 2013.
  • Copeland, S. R., Lonkar, A. K., Palacios, F., and Alonso, J. J., "Adjoint-Based Goal-Oriented Mesh Adaptation for Nonequilibrium Hypersonic Flows," 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, AIAA Paper 2013-0552, Grapevine, TX, Jan. 2013.
  • Economon, T. D., Palacios, F., Alonso, J. J., "Unsteady Aerodynamic Design on Unstructured Meshes with Sliding Interfaces and Active Flow Control," 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, AIAA Paper 2013-0632, Grapevine, TX, Jan. 2013.
  • Lukaczyk, T., Taylor, T., Palacios, F., and Alonso, J. J., "Managing Gradient Inaccuracies while Enhancing Response Surface Models," 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, AIAA Paper 2013-1042, Grapevine, TX, Jan. 2013.

 

The following reports, articles, and texts were used as reference material during the implementation of the SU2 suite. Please see these references for more detail on particular components of the code:

  • Barth, T., Numerical Methods for Conservative Laws on Structured and Unstructured Meshes, VKI March 2003 Lecture Series.
  • Hirsch, C., Numerical Computation of Internal and External Flows, Volume 2, John Wiley and Sons, 1990.
  • Jameson, A., Analysis and Design of Numerical Schemes for Gas Dynamics 1 Artificial Diffusion, Upwind Biasing, Limiters and Their Effect on Accuracy and Multigrid Convergence, RIACS Technical Report 94.15, International Journal of Computational Fluid Dynamics, Vol. 4, 1995, pp. 171-218.
  • Jameson, A., Analysis and Design of Numerical Schemes for Gas Dynamics 2 Artificial Diffusion and Discrete Shock Structure, RIACS Report No. 94.16, International Journal of Computational Fluid Dynamics, Vol. 5, 1995, pp. 1-38.
  • Jameson, A., The present status, challenges, and future developments in computational fluid dynamics, AGARD, editor, Progress and challenges in CFD methods and algorithms, 1995.

  • Jameson, A., Aerodynamic design via control theory. Journal of Scientific Computing, 3:233–260, 1988.

  • Jameson, A., Aerodynamic shape optimization using the adjoint method. In Lecture Notes Presented at the VKI Lecture Series, Rhode Saint Genese Begium, 2 2003. Von karman Institute for fluid dynamics.

  • Jameson, A. and Kim, S., Reduction of the adjoint gradient formula for aerodynamic shape optimization problems. AIAA Journal, 41(11):2114–2129, 2003.

  • Jameson, A. and Schmidt, W. and Turkel, E., Numerical solution of the Euler equations by finite volume methods using Runge-Kutta time stepping schemes. AIAA Paper, 81-1259, 1981.

  • Karypis, G. and Kumar, V., A fast and high quality multilevel scheme for partitioning irregular graphs, International Conference on Parallel Processing, pp 113-122, 1995
  • LeVeque, R. J., Numerical Methods for Conservation Laws, Birkhauser Verlag, 2006, Lectures in Mathematics.
  • Mavriplis, D., On convergence Acceleration Techniques for Unstructured Meshes, ICASE Report No, 98-44.
  • Quarteroni, A. and Valli, A., Numerical approximation of partial differential equations, Springer Series in Computational Mathematics. Springer, 1997.
  • Sethian, J., Level Set Methods and Fast Marching Methods, Cambridge University Press, 1999.
  • Toro, E. F., Riemann Solvers and Numerical Methods for Fluid Dynamics: a Practical Introduction, Springer-Verlag, 1999.
  • Wesseling, P., Principles of Computational Fluid Dynamics, Springer Series in Computation Mathematics, Springer, 2000.

  • R. W. MacCormack and D. D'Ambrosio and D.Giordano and J. K. Lee and T. Kim, Plasmadynamic Simulations with Strong Shock Waves, AIAA, 2011.

  • M. I. Hoffert and H. Lien, Quasi-One Dimensional Nonequilibrium Gas Dynamics of Partially Ionized Two-Temperature Argon, Physics of Fluids, 1967.

  • Spalart, P. R. and Allmaras, S. R., "A One-Equation Turbulence Model for Aerodynamic Flows," Recherche Aerospatiale, No. 1, 1994, pp. 5-21.
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