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Publication List for Thomas H. Pulliam
Latest Update December 2008
  1. Pulliam, T. H. ,A Numerical Algorithm for the Prediction of Long-Term Stratospheric Circulation, Ph. D. Thesis, Stanford University, 1976

  2. Pulliam T. H. and Steger J. L., On Implicit Finite-Difference Simulations of Three- Dimensional Flow, AIAA Journal, Vol 18, No. 2 1980 p. 159, also AIAA Paper No. 78-10 Jan. 1978

  3. Kutler P. , Pulliam T. H. and Vigneron, Y. C., Computation of the Viscous Supersonic Flow Over External Axial Corners, AIAA J. , Vol 17, No 6, 1979, p. 571, also AIAA Paper No. 78-1135, July 1978

  4. Nietubicz C. J. , Pulliam T. H. and Steger J. L., Numerical Solution of the Azimuthal- Invariant Thin- Layer Navier- Stokes Equations ,AIAA J., Vol 18, No 12, 1980 p. 1411, also AIAA Paper No. 79-0010, Jan. 1979 and Technical Report ARBRL-TR-02227 March 1980

  5. Pulliam T. H. and Lomax H., Simulation of Three- Dimensional Compressible Viscous Flow on the Illiac IV Computer, AIAA Paper No. 79-0206, 1979

  6. Steele C. R., Ranjan G. V., Goto C. and Pulliam T. H., Computer Analysis of Shells of Revolution Using Asymptotic Results, Proceedings of AIAA 20th Structural Dynamics and Materials Conference, St. Louis, Mo., April 1979

  7. Steele C. R. , Ranjan G. V. , Goto C. and Pulliam T. H., FAST - A Shell Code Using Asymptotic Results, Proceedings of the 5th Structural Mechanics Conference in Reactor Technology, Berlin, 1979

  8. Kutler P. , Pedelty J. A. , and Pulliam T. H., Supersonic Flow Over Three- Dimensional Ablated Nosetips Using an Unsteady Implicit Numerical Procedure, AIAA Paper No. 80-63, 1980.

  9. Chaussee D. S. and Pulliam T. H., Two- Dimensional Inlet Simulation Using a Diagonal Implicit Algorithm, AIAA J., Vol 19, 1981 p. 153, also AIAA Paper No. 80-67, Jan. 1980

  10. Steger J. L. , Pulliam T. H. and Chima R. V., An Implicit Finite Difference Code for Inviscid and Viscous Cascade Flow, AIAA Paper No. 80-1427, 1980

  11. Chaussee D. S. , Kutler P. and Pulliam T. H., Three Dimensional Viscous Flow Field Program, Part 1: Viscous Blunt Body Program , FSI Report No. 80-08, 1980

  12. Pulliam T. H. and Chaussee D. S.,A Diagonal Form of an Implicit Approximate Factorization Algorithm, Journal of Computational Physics, Vol 39, No. 2, Feb. 1981

  13. Chaussee D. S., Patterson J. L., Kutler P. , Pulliam T. H. and Steger J. L. ,A Numerical Simulation of Hypersonic Viscous Flows over Arbitrary Geometries at High Angle of Attack, AIAA Paper No. 81-0050, 1981

  14. Lomax H., Pulliam T. H. and Jespersen D. C., Eigensystem Analysis Techniques for Finite- Difference Equations. 1. Multi- level Techniques ,AIAA Paper No. 81-1027, 1981

  15. Pulliam T. H.,Characteristic Boundary Conditions for the Euler Equations, Proceeding of Symposium on Numerical Boundary Condition Procedures NASA CP 2201, 1981 p. 165

  16. Lomax H. and Pulliam T. H., A Three- Dimensional Implicit Code for the Illiac IV, Series in Computational Physics on Parallel Computations, Pub. Editor Garry Rodrigue, Academic Press, New York , N. Y. 1982

  17. Lasinski T. A., Andrews A. E., Sorenson R. L., Chaussee D. S., Pulliam T. H., and Kutler P., Computation of the Steady Viscous Flow Over a Tri- Element Augmentor Wing Airfoil, AIAA Paper No. 82-0021, 1982

  18. Hessenius K. A. and Pulliam T. H., A Zonal Approach to the Solution of the Euler Equations, AIAA Paper No. 82-0969, 1982

  19. Pulliam, T. H., Jespersen, D. C., and Childs, R. E. , An Enhanced Version of an Implicit Code for the Euler Equations, AIAA Paper No. 83-0344, 1983

  20. Jespersen, D. C. and Pulliam, T. H., Approximate Newton Methods and Flux Vector Splitting, AIAA Paper No. 83-1899, 1983

  21. Chow, L. J., Pulliam, T. H. and Steger, J. L., A General Perturbation Approach for Computational Fluid Dynamics , AIAA J.,Vol 22, No. 12, (also AIAA Paper No. 83-1903, 1983), 1984, p.1748

  22. Pulliam, T. H. , Implicit Finite- Difference Methods for the Euler Equations, Advances in Computational Transonics Fourth Volume in the Series on Recent Advances in Numerical Methods in Fluids, Editor W. G. Habashi,addr Pineridge Press Ltd, 1983

  23. Childs, R. E. and Pulliam, T. H. , A Newton Multigrid Method for the Euler Equations, AIAA Paper No. 84-0430, 1984

  24. Flores, J., Barton, J., Holst, T. and Pulliam, T. , Comparison of the Full Potential and Euler Formulations For Computing Transonic Airfoil Flows, Presented at the 9th International Conference on Numerical Methods in Fluid Dynamics, Saclay, France, June 1984, Lecture Notes in Physics Vol 218, No. 5, Editor Soubbaramayer and J. Boujot, Springer-Verlag, 1985

  25. Barton, J. T. and Pulliam, T. H., Airfoil Computation at High Angles of Attack, Inviscid and Viscous Phenomena,AIAA J. Vol. 24, No. 5, (also AIAA Paper No. 85-0524, 1984) 1986 p. 705

  26. Pulliam, T. H. , Euler and Thin Layer Navier Stokes Codes : ARC2D, ARC3D, Computational Fluid Dynamics, A workshop Held at the University of Tennessee Space Institute, UTSI publ. E02-4005-023-84, 1984

  27. Pulliam T. H. and Steger, J. L. , Recent Improvements in Efficiency, Accuracy, and Convergence for Implicit Approximate Factorization Algorithms, AIAA Paper 85-0360, AIAA 23rd Aerospace Sciences Meeting, Reno, Nev., Jan. 1985

  28. Pulliam, T. H. and Barton, J. T., Euler Computations of AGARD Working Group 07 Airfoil Test Cases, AIAA Paper 85-0018, AIAA 23rd Aerospace Sciences Meeting, Reno Nev., 1985

  29. Pulliam, T.H., Efficient Solution Methods for The Navier-Stokes Equations, Lecture Notes for the von Kármán Institute For Fluid Dynamics Lecture Series : Numerical Techniques for Viscous Flow Computation In Turbomachinery Bladings, von Kármán Institute, Rhode-St-Genese, Belgium , 1985

  30. Pulliam T. H., Artificial Dissipation Models for the Euler Equations, AIAA J., Vol 24, No 12 p. 1931 (also AIAA Paper 85-0438, AIAA 23rd Aerospace Sciences Meeting, Reno, Nev., Jan. 1985), 1986

  31. Barth, T. J., and Pulliam T. H., Navier- Stokes Computations For Exotic Airfoils, AIAA Paper 85-0109, AIAA 23rd Aerospace Sciences Meeting, Reno, Nev., Jan. 1985 (Accepted AIAA J. 1987)

  32. Pulliam T. H. , Jespersen, D. C., and Barth, T. J., Navier- Stokes Computations For Circulation Controlled Airfoils, AIAA Paper 85-1587, AIAA 18th Fluid and Plasma Dynamics Conference Cincinnati, Ohio, July 1985

  33. Pan, D. and Pulliam, T. H., The Computation Of Steady 3-D Separated Flows Over Aerodynamic Bodies At Incidence And Yaw, AIAA Paper No. 86-0109, AIAA 24rd Aerospace Sciences Meeting, Reno, Nev., Jan. 1986

  34. Pulliam, T. H., Implicit Solution Methods In Computational Fluid Dynamics, Applied Numerical Mathematics, Vol 2, No. 6, North-Holland Elsevier Science Publishers B. V., Amsterdam, The Netherlands, Dec. 1986 p. 441

  35. Maksymiuk, C. M. and Pulliam, T. H. , Viscous Transonic Airfoil Workshop Results Using ARC2D, AIAA Paper No. 87-0415, AIAA 25rd Aerospace Sciences Meeting, Reno, Nev., Jan. 1987

  36. Pulliam, T.H., Implicit Methods in CFD , Numerical Methods for Fluid Dynamics III, The Institute of Mathematics and Its Publications Conference Series, Proceeding of the ICFD 1988 Conference on Numerical Methods for Fluid Dynamics, University of Oxford, UK, March 1988, Ed. K. W. Morton and M. J. Baines, Clarendon Press, Oxford, England

  37. Cheer, A.Y., Saleem, M., Pulliam, T.H. and Hafez, M., Analysis of the Convergence History of Flow Through Nozzles with Shocks AIAA Paper No. 88-3795, 1st National Fluid Dynamics Congress, Cincinnati, Ohio, July 1988

  38. Pulliam, T.H., Low Reynolds Number Numerical Solutions of Chaotic Flow, AIAA paper 89-0123, AIAA 27th Aerospace Sciences Meeting, Reno, NV, 1989

  39. Pulliam, T.H., A Computational Challenge : Euler Solution for Ellipses, AIAA J., Vol. 28,No. 10, Oct. 1990, also AIAA paper 89-0469, AIAA 27th Aerospace Sciences Meeting, Reno, NV, 1989

  40. Pulliam, T. H. and Vastano, J. A. Numerical Simulation Of Chaotic Flows: Measures of Chaos, ASME Publication FED-Vol. 77, $3^{rd}$ Joint ASCE/ASME Mechanics Conference Forum on Chaotic Flows, La Jolla, CA, 1989

  41. Pulliam, T. H., Introduction to Chaos Theory in CFD, AIAA 90-1440, AIAA 21st Fluid Dynamics, Plasma Dynamics, and Lasers Conference, Seattle, WA, June 1990.

  42. Pulliam, T. H. and Vastano, J. A., Chaotic Flow Over An Airfoil, 12th International Conference on Numerical Methods in Fluid Dynamics, July 9-13, 1990, U. of Oxford, England.

  43. Maksymiuk, C.M., Swanson, R.C., and Pulliam, T.H., 1990, A Comparison of Two Central Difference Schemes for Solving the Navier-Stokes Equations, NASA TM 102815

  44. Shariff, K., Pulliam, T.H. and Ottino, J.M., 1991, A Dynamical Systems Analysis of Kinematics in the Time-Periodic Wake of a Circular Cylinder, AMS Lectures in Applied Mathematics, Vol. 28, pp 613.

  45. Saleem, M., Pulliam, T.H. and Cheer, A.Y., Convergence Acceleration and Spectrum Transformation of a Two Dimensional Fluid Flow Problem, J Comp Physics, Vol. 104, No. 1, pp. 1-13, 1993.

  46. Pulliam, T. H. and Vastano,J. A., Transition To Choas In An Open Unforced 2-D Flow, J Comp Physics, Vol. 105 No. 1, PP.133-149 1993.

  47. Chan, W.M., Shariff, K., and Pulliam, T.H.,Instabilities of Two-Dimensional Inviscid Compressible Vorticies, J Fluid Mechanics, Vol. 253, pp 173-209, Aug. 1993.

  48. Pulliam, T.H.,Time Accuracy And The Use Of Implicit Methods,AIAA Paper 93-3360, Presented at AIAA $11^{th}$ Computational Fluid Dynamics Conference, Orlando, FL, July 1993.

  49. Rogers, S.E. and Pulliam, T.H.,Accuracy Enhancements For Overset grids Using a Defect Correction Approach ,AIAA Paper 94-0523, Presented at AIAA $32^{nd}$ Aerospace Sciences Meeting Reno, NV, Jan. 1994.

  50. Eggleton, C., Ferziger, J., Pulliam, T.,Moderate Reynolds Number Entry Flow and Boundary Layer Approximations For a Viscoelastic Fluid, Physics of Fluids A, Feb. 1994.

  51. Gooch, C.F., MacCormack, R.W., Pulliam, T.H., Solution of the Navier-Stokes Equations Using State-vector Splitting, Submitted J. of Comp. Physics, 1994.

  52. Feng, D., Pulliam, T.H., Tensor-GMRES Method For Large Sparse System of Nonlinear Equations, SIAM Journal of Optimization,Vol. 7, Issue 3, Aug. 1997. also RIACS Tech. Report 94.12, 1994

  53. Eggleton, C., Pulliam, T., and Ferziger, J., Numerical Simulation of Viscoelastic Flow using Flux Difference Splitting at Moderate Reynolds Number, Journal of Non-Newtonian Fluid Mechanics, 64, pp 269-298, 1996.

  54. Pulliam, T., Rogers, S., Barth, T., Practical Aspects of Krylov Subspace Based - Iterative Methods In CFD,AGARD 77th Fluid Dynamics Panel Symposium on Progress and Challenges in CFD Methods and Algorithms, Seville, Spain, 2-5 October 1995

  55. Feng, D., Pulliam, T.H., An All-At-Once Reduced Hessian SQP Scheme For Aerodynamics Design Optimization, RIACS Tech. Report 95-19, 1995

  56. Feng, D., Pulliam, T.H., Aerodynamic Design Optimization Via Reduced Hessian SQP With Solution Refining, RIACS Tech. Report 95-24, 1995

  57. Pulliam, T., Implicit Methods for the Euler Equations, Handbook of Fluid Dynamics and Fluid Machinery, Vol. 2, pp. 1420-1430, Eds. J. Schetz and A. Fuhs, Pub. John Wiley and Sons, New York, 1996.

  58. Jespersen, D., Pulliam, T.H., and Buning, Recent Enhancement to OVERFLOW, AIAA paper 97-0644 Presented at AIAA $35^{nd}$ Aerospace Sciences Meeting Reno, NV, Jan. 1997.

  59. Rothe, P., Johnson, J., Barry, J., and Pulliam, T.,CFD Assessment with Difuser Data, FEDSM97-3026, 1997 ASME Fluids Engineering Division Summer Meeting, June 22-26, 1997.

  60. MacCormack, R.W. and Pulliam, T., Assessment Of A New Numerical Procedure For Fluid Dynamics, AIAA paper 98-2821 Presented at the 29th AIAA Fluid Dynamics Conference, Albuquerque, New Mexico, June 15-18, 1998.

  61. Pulliam, T., MacCormack, R.W. and Venkateswaran, S, Convergence Characteristics of Various Approximate Factorizations, Lecture Notes in Physics, Sixteenth International Conference on Numerical Methods in Fluid Dynamics, ISBN 1616-6361, Springer, Vol. 515, 1998.

  62. Delanaye, M., Aftosmis, M.J., Berger, M.J., Liu, Y., and Pulliam, T.H., Automatic Hybrid-Cartesian Grid Generation for High Reynolds Number Flows Around Complex Geometries,AIAA 99-0777 Presented at 37th AIAA Aerospace Sciences Meeting, Reno, NV, Jan. 1999.

  63. Zingg, D.W., De Rango, S., Numec, M., and Pulliam, T.H., Comparison of Several Spatial Descretizations for the Navier-Stokes Equations, JCP 160, pp 683-704, 2000, also AIAA 99-3260, Presented at the 14th AIAA Computational Fluid Dynamics Conference, Norfolk, VA, July 1999.

  64. Pulliam, T.H., Kutler, K. and Rossow, V, Harvard Lomax: His Quiet Legacy to CFD, Presented at the 14th AIAA Computational Fluid Dynamics Conference, Norfolk, VA, July 1999.

  65. Lomax, H., Pulliam, T.H. and Zingg, D.W., Fundamentals of Computational Fluid Dynamics, Scientific Computation, Spinger-Verlag, Berlin, 2001. 249 pp. ISBN 3-540-41607-2

  66. Walsh, Paul C. and Pulliam,Thomas H. The Effect of Turbulence Model Solution on Viscous Flow Problems AIAA 2001-1018, AIAA Aerospace Sciences Meeting, Reno NV, Jan. 2001

  67. Holst, Terry L. and Pulliam,Thomas H. Aerodynamic Shape Optimization Using A Real-Number-Encoded Genetic Algorithm AIAA 2001-2473, June, 2001

  68. Nemec, M., Zingg, D.W., and Pulliam, T.H., Multi-Point and Multi-Objective Aerodynamic Shape Optimization, AIAA Paper 2002-5548, 9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Atlanta, Sept. 2002. Also AIAA Journal 2004, Vol. 42 No 6. 1057-1065

  69. Holst, T. L. and Pulliam, T. H., Transonic Wing Shape Optimization Using a Genetic Algorithm, Presented at Symposium Transsonicum IV, Göttingen, Germany, September 2-6, 2002.

  70. Pandya, S.A., Venkateswaran, S., Pulliam, T.H., Implementation of Preconditioned Dual-Time Procedures in OVERFLOW AIAA 2003-0072, AIAA 41st Aerospace Sciences Meeting, Reno, NV, Jan 2003.

  71. Pulliam, T.H., Nemec, M., Holst, T.L. and Zingg, D.W. Comparison of Genetic and Adjoint Methods for Multi-Objective Viscous Airfoil Optimizations AIAA 2003-0298, AIAA 41st Aerospace Sciences Meeting, Reno, NV, Jan 2003.

  72. Holst, T. L and Pulliam, T. H., Evaluation of Genetic Algorithm Concepts Using Model Problems, Part I: Single-Objective Optimization, NASA/TM-2003-212812, December 2003.

  73. Holst, T. L and Pulliam, T. H., Evaluation of Genetic Algorithm Concepts Using Model Problems, Part II: Multi-Objective Optimization, NASA/TM-2003-212813, December 2003.

  74. Nemec, M., Aftosmis, M., and Pulliam T., CAD-Based Aeroynamic Design of Complex Configurations Using a Cartesian Method Computational Fluid Dynamics 2004, Proceedings of the Third International Conference on Computational Fluid Dynamics, ICCFD 3, Toronto, 12-16 July 2004, Eds. C. Groth and D. W. Zingg, Springer-Verlag, Berlin, 2006, pg. 699-704 Also:AIAA 2004-0113, AIAA 42st Aerospace Sciences Meeting, Reno, NV, Jan 2004.

  75. Nemec, M., Aftosmis, M., Murman, S., and Pulliam T., Adjoint Formulation for an Embedded-Boundary Cartesian Method $43^{rd}$ AIAA Aerospace Sciences Meeting, Jan 2005, Reno NV also NAS Tecnical Report, nas-05-008, NASA Ames Research Center, 2005.

  76. Nelson, A., Nemec, M., Aftosmis, M., and Pulliam T., Aerodynamic Design Optimization of Rocket Control Surface Geometery Using Cartesian Methods and CAD Geometry AIAA 2005-2836$23^{rd}$ AIAA Applied Aerodynamics Conference, Toronto, CA, June 2005.

  77. Nelson, A., Alonso, J., and Pulliam T., Multi-Fidelity Aerodynamic Optimization Using Treed Meta-Models AIAA 2007-4057$25^{rd}$ AIAA Applied Aerodynamics Conference, Miami, FL, June 2007.

  78. Zingg, D.W. Nemec, M., Pulliam, T.H., A Comparative Evaluation of Genetic and Gradient-based Algorithms Applied to Aerodynamic Optimization Revue Européenne de Mécanique Numérique, Vol. 17/1-2, pp 103-126, European Journal of Computational Mechanics, 2008.

  79. Wissink, A.M., Sitaraman, J., Sankaran, V., Mavriplis, D.J., Pulliam, T.H., A Multi-Code Python-Based Infrastructure for Overset CFD with Adaptive Catresian Grids AIAA 2008-0927, AIAA 46th Aerospace Sciences Meeting, Reno, NV, Jan 2008.

  80. Potsdam M., Pulliam, T.H.,Turbulence Modeling Treatment for Rotocraft Wakes Presented at AHS Aeromechanics Specialist's Meeting, San Francisco, CA, Jan. 23-25, 2008

  81. Pulliam, T.H.,Early Development of Implicit Methods for Computational Fluid Dynamics at NASA Ames Computers & Fluids, 38, p 491-495, 2008


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Thomas H. Pulliam 2008-12-22