A Rapid, Robust, and Accurate Coupled Boundary-Layer Method for Cart3D
Rodriguez, D. L., Sturdza, P., Suzuki, Y., Martins-rivas, H., Peronto, A., 50th AIAA Aerospace Sciences Meeting and Exhibit, AIAA-2012-0302, Nashville, Tennessee, Jan. 2012.
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A Quasi-Simultaneous Interactive Boundary-Layer Model for a Cartesian Euler Solver
Sturdza, P., Suzuki, Y., Martins-rivas, H., Rodriguez, D. L., 50th AIAA Aerospace Sciences Meeting and Exhibit, AIAA-2012-0303, Nashville, Tennessee, Jan. 2012.
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Improving the Accuracy of Euler/Boundary-Layer Solvers with Anisotropic Diffusion Methods
Rodriguez, D. L., Sturdza, P., Eymard, R., 50th AIAA Aerospace Sciences Meeting and Exhibit, AIAA-2012-0304, Nashville, Tennessee, Jan. 2012.
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Extensible Rapid Transition Prediction for Aircraft Conceptual Design
Rajnarayan, D., Sturdza, P., 29th AIAA Applied Aerodynamics Conference, AIAA-2011-3813, Honolulu, Hawaii, Jun. 2011.
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A More Efficient Conceptual Design Process Using the RAGE Geometry Modeler
Suwaratana, D. L., Rodriguez, D. L., 49th AIAA Aerospace Sciences Meeting and Exhibit, AIAA-2011-0159, Orlando, Florida, Jan. 2011.
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Aircraft Conceptual Design with Natural Laminar Flow
Allison, E., Kroo, I., Sturdza, P., Suzuki, Y., Martins-Rivas, H., 27th International Congress of the Aeronatuical Sciences, Nice, France, Sep. 2010.
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Propulsion/Airframe Integration and Optimization on a Supersonic Business Jet
Rodriguez, D. L., 45th AIAA Aerospace Sciences Meeting and Exhibit, AIAA-2007-1048, Reno, Nevada, Jan. 2007.
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Extensive Supersonic Natural Laminar Flow on the Aerion Business Jet
Sturdza, P., 45th AIAA Aerospace Sciences Meeting and Exhibit, AIAA-2007-0685, Reno, Nevada, Jan. 2007.
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Conceptual Design of Conventional and Oblique Wing Configurations for Small Supersonic Aircraft
Wintzer, M., Sturdza, P., and Kroo, I. M., 44th AIAA Aerospace Sciences Meeting and Exhibit, AIAA-2006-0930, Reno, Nevada, Jan. 2006.
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A Rapid Geometry Engine for Preliminary Aircraft Design
Rodriguez, D. L. and Sturdza, P., 44th AIAA Aerospace Sciences Meeting and Exhibit, AIAA-2006-0929, Reno, Nevada, Jan. 2006.
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Two-Level Multi-Fidelity Design Optimization Studies for Supersonic Jets
Choi, S., Alonso, J.J., Kim, S., Kroo, I., and Wintzer, M., 43rd Aerospace Sciences Meeting and Exhibit, AIAA Paper 2005-0531, Reno, Nevada, January 10-13 2005.
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A Framework for Aircraft Conceptual Design and Environmental Performance Studies
Antoine, N., Kroo, I., Willcox, K., and Barter, G., AIAA paper 2004-4314, 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Albany, NY, 30 Aug. Sept. 2004.
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Multi-Fidelity Design Optimization of Low-Boom Supersonic Business Jets
Choi, S., Alonso, J. J., Kroo, I., and Wintzer, M., AIAA paper 2004-4371, 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Albany, NY, 30 Aug. Sept. 2004.
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An Aerodynamic Design Method for Natural Laminar Flow Aircraft
Sturdza, P., Ph.D. Dissertation, Stanford University, Dec. 2003.
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The Complex-Step Derivative Approximation
Martins, J. R. R. A., Sturdza, P., Alonso, J. J., ACM Trans. on Math. Softw., Vol 29, Issue 3, Sept. 2003.
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Multidisciplinary Optimization of a Supersonic Inlet Using a Cartesian CFD Method
Rodriguez, D. L., AIAA paper 2004-4492, Aug. 2004.
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Response Surface Based Optimization with a Cartesian CFD Method
Rodriguez, D. L., AIAA paper 2003-0465, Jan. 2003.
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A Multidisciplinary Optimization Method for Designing Boundary Layer Ingesting Inlets
Rodriguez, D. L., AIAA paper 2002-5665, Sept. 2002.
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Multidisciplinary Optimization Method for Designing Boundary-Layer Ingesting Inlets
Rodriguez, D. L., Ph.D. Dissertation, Stanford University, Jan. 2001.
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A Multidisciplinary Optimization Method for Designing Inlets Using Complex Variables
Rodriguez, D. L., AIAA paper 2000-4875, Sept. 2000.
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