All Stories

  1. Direct Optimization of Sonic Boom Ground Noise via a Coupled-Adjoint Method

    Article • Journal of Aircraft, April 2026, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. David L Rodriguez

  2. Sonic Boom Ground Noise Minimization via the Adjoint Method

    Article • January 2025, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. David L Rodriguez, Sriram Rallabhandi

  3. Goal-Oriented Discretization Error Control in Coupled Nearfield-Farfield Low-Boom Simulations

    Article • June 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Sriram Rallabhandi, Dr. David L Rodriguez

  4. Adjoint-Based Mesh Adaptation and Shape Optimization for Simulations with Propulsion

    Article • June 2019, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. David L Rodriguez

  5. Distributed-Flap Layout Trade Study on a Highly Flexible Common Research Model

    Article • June 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. David L Rodriguez

  6. Formulation and Implementation of Inflow/Outflow Boundary Conditions to Simulate Propulsive Effects

    Article • January 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. David L Rodriguez

  7. Optimization of Flexible Wings with Distributed Flaps at Off-Design Conditions

    Article • Journal of Aircraft, November 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. David L Rodriguez

  8. Optimized Off-Design Performance of Flexible Wings with Continuous Trailing-Edge Flaps

    Article • January 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. David L Rodriguez

  9. Static Aeroelastic Analysis with an Inviscid Cartesian Method

    Article • January 2014, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. David L Rodriguez

  10. A Rapid, Robust, and Accurate Coupled Boundary-Layer Method for Cart3D

    Article • January 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. David L Rodriguez

  11. Improving the Accuracy of Euler/Boundary-Layer Solvers with Anisotropic Diffusion Methods

    Article • January 2012, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. David L Rodriguez

  12. A More Efficient Conceptual Design Process Using the RAGE Geometry Modeler

    Article • January 2011, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. David L Rodriguez

  13. Multidisciplinary Optimization Method for Designing Boundary-Layer-Ingesting Inlets

    Article • Journal of Aircraft, May 2009, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. David L Rodriguez

  14. Propulsion/Airframe Integration and Optimization on a Supersonic Business Jet

    Article • January 2007, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. David L Rodriguez

  15. A Rapid Geometry Engine for Preliminary Aircraft Design

    Article • January 2006, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. David L Rodriguez

  16. Multidisciplinary Optimization of a Supersonic Inlet Using a Cartesian CFD Method

    Article • August 2004, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. David L Rodriguez

  17. Response Surface Based Optimization with a Cartesian CFD Method

    Article • January 2003, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. David L Rodriguez

  18. A Multidisciplinary Optimization Method for Designing Boundary Layer Ingesting Inlets

    Article • September 2002, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. David L Rodriguez

  19. A multidisciplinary optimization method for designing inlets using complex variables

    Article • September 2000, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. David L Rodriguez

  20. A 3D multidisciplinary design method for boundary layer ingesting inlets

    Article • January 2000, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. David L Rodriguez

  21. A 2D multidisciplinary design method for boundary layer ingesting inlets

    Article • January 1999, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. David L Rodriguez

  22. Validation of CFD methods for a boundary later ingesting inlet

    Article • January 1998, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. David L Rodriguez