All Stories

  1. Effects of Nonlinear Structural Damping Uncertainty on F-16 Limit Cycle Oscillations

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

    Dr. Zhichao zhang

  2. FUN3D-based Adjoint Sensitivity for Elastic Tandem Airfoils in Chaotic Flows

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

    Dr. Zhichao zhang

  3. CFD-based Aeroelastic Adjoint Sensitivities for Flight Vehicle Weight Minimization Using Sizing and Shape Design Variables

    Article • January 2017, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Zhichao zhang

  4. Adjoint Based Structure and Shape Optimization with Flutter Constraints

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Zhichao zhang

  5. Nonlinear Aerodynamics and Nonlinear Structures Interaction for F-16 Limit Cycle Oscillation Prediction

    Article • January 2016, American Institute of Aeronautics and Astronautics (AIAA)

    Dr. Zhichao zhang

  6. Design-Oriented Computational Fluid Dynamics-Based Unsteady Aerodynamics for Flight-Vehicle Aeroelastic Shape Optimization

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

    Dr. Zhichao zhang

  7. Unsteady Aerostructure Coupled Adjoint Method for Flutter Suppression

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

    Dr. Zhichao zhang