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2001 |
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Chung, H.S., and Alonso, J.J., "Using Gradients to Construct Response
Surface Models for High-Dimensional Design Optimization Problems", AIAA 39th Aerospace Sciences Meeting
and Exhibit,AIAA-2001-0922, Reno, NV, January 8-11, 2001.
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Legresley, P.A., and Alonso, J.J., "Investigation of Non-Linear Projection for POD
Based Reduced Order Models for Aerodynamics", AIAA 39th Aerospace Sciences Meeting and Exhibit,AIAA-2001-0926,
Reno, NV, January 8-11, 2001.
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Jameson, A., Vassberg, J., "Computational Fluid Dynamics (CFD) for
Aerodynamic Design: Its Current and Future Impact", AIAA 39th Aerospace Sciences Meeting
and Exhibit,AIAA-2001-0538, Reno, NV, January 8-11, 2001.
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Martins, J. and Alonso, J.J., "A Connection Between the Complex-Step Derivative
Approximation and Algorithmic Differentiation", AIAA 39th Aerospace Sciences Meeting and Exhibit,AIAA-2001-0921,
Reno, NV, January 8-11, 2001.
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McMullen, M.S., Jameson, A. and Alonso, J.J., "Acceleration of Convergence
to a Periodic Steady State in Turbomachinery Flows", AIAA 39th Aerospace Sciences Meeting
and Exhibit,AIAA-2001-0152, Reno, NV, January 8-11, 2001.
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Shankaran, S., et. al., "A Multi-Code-Coupling Interface for Combustor
Turbomachinery Simulations", AIAA 39th Aerospace Sciences Meeting and Exhibit,AIAA-2001-0974,
Reno, NV, January 8-11, 2001.
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Yao, J., Davis, R., Jameson, A. and Alonso, J.J., "Unsteady Flow Investigation
in Axial Turbines Using the Massively Parallel Flow Solver TFLO", AIAA 39th Aerospace Sciences Meeting
and Exhibit,AIAA-2001-0529, Reno, NV, January 8-11, 2001.
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2000 |
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LeGresley, P.A, and Alonso, J.J., "Airfoil Design Optimization Using
Reduced Order Models Based on Proper Orthogonal Decomposition," Fluids
2000 Conference and Exhibit, AIAA-2000-2545, Denver, CO, June 19-22, 2000.
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LeGresley, P.A., et. al., "1998/1999 AIAA Foundation Graduate Team
Aircraft Design Competition: Super STOL Carrier On-board Delivery
Aircraft," World Aviation Congress & Exhibition, San Diego, CA, October
10-12, 2000, SAE 00WAC-16.
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Martins, J. R. R. A., I.M.Kroo and J.J.Alonso,
"An Automated Method for Sensitivity Analysis using Complex Variables"
Proceedings of the 38th Aerospace Sciences
Meeting, AIAA Paper 2000-0689, Reno, NV, January 2000.
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Nadarajah, Siva, Jameson, Antony, "A Comparison of the Continuous and
Discrete Adjoint Approach to Automatic Aerodynamic Optimization," AIAA 38th Aerospace Sciences
Meeting and Exhibit, AIAA-2000-0667, Reno, NV, January 2000.
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1999 |
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Jameson, A., A Perspective on Computational Algorithms for Aerodynamic Shape Analysis and Design, Sixth Taiwan
National Conference on Computational Fluid Dynamics, Taitung, Taiwan ROC, August 1999.
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LeGresley, P. et al., "The Cardinal, A Graduate Team Aircraft Design," 1999 AIAA Graduate Team Aircraft Proposal, June 1 1999.
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Reuther, J., J. J. Alonso, J. R. R. A. Martins, S. C. Smith,
"A Coupled Aero-Structural Optimization Method for Complete Aircraft
Configurations",
Proceedings of the 37th Aerospace Sciences
Meeting, AIAA Paper 99-0187, Reno, NV, January 1999.
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1998 |
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Jameson, A., Alonso, J.J., Reuther, J. Martinelli, L., Vassberg, J.C., Aerodynamic Shape Optimization
Techniques Based on Control Theory, AIAA 29th Fluid Dynamics Conference, AIAA 98-2538, Albuquerque, NM, June 15-18, 1998.
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Jameson, A., Pierce, N., Martinelli, L., Optimum Aerodynamic Design using the Navier Stokes Equation, Theoretical
and Computational Fluid Dynamics, Vol. 10, pp213-237, 1998.
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1997 |
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Jameson, A., Pierce, N., Martinelli, L., Optimum Aerodynamic Design using the Navier-Stokes Equation, AIAA 35th Aerospace
Sciences Meeting and Exhibit, AIAA 97-0101, Reno, NV, January 1997.
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1996 |
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Jameson, A, Alonso, J.J., Automatic Aerodynamic Optimization on Distributed Memory Architechtures,
AIAA 34th Aerospace Sciences Meeting and Exhibit, AIAA Paper 96-0409, Reno, NV, January 1996.
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1995 |
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Alonso, J.J., Marinelli, Luigi, Jameson, A., Multigrid Unsteady Navier-Stokes Calculations with Aeroelastic Applications,
AIAA 33rd Aerospace Sciences Meeting and Exhibit, AIAA Paper 95-0048, Reno, NV, January 1995.
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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, pp171-218, 1995.
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Jameson, A., Analysis and Design of Numerical Schemes for Gas
Dynamics 2 Artificial Diffusion, Upwind Biasing, Limiters and Their Effect on Accuracy and Multigrid Convergence,
RIACS Technical Report 94.16, International Journal of Computational Fluid Dynamics, Vol 5, pp1-38, 1995.
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Jameson, A., The Present Status, Challenges, and Future Developments in Computational Fluid Dynamics,
Proceedings of the 7th AGARD Fluid Dynamics Panel Symposium, Seville, October 1995.
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1994 |
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Alonso, J.J., Jameson, A.,"Fully-Implicit Time-Marching Aeroelastic Solutions," AIAA 32nd Aerospace Sciences Meeting and Exhibit, AIAA Paper 94-0056, Reno, NV, January 1994. |
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Alonso, J.J., Mitty, T.J., Martinelli, L., Jameson, A., A Two-Dimensional Multigrid Navier-Stokes Solver for Multiprocessor
Architectures, Proceedings of Parallel CFD '94, Kyoto May 1994, Parallel Computational Fluid Dynamics: New ALgorithms and Applications (ed. Satofuka, Periaux, Ecer), Elsevier Science B.V., 1995.
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