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  1. Supersonic Configurations at Low Speeds (SCALOS): Results and Insights from the 2024 Wind Tunnel Test Campaign

    Article • January 2026, American Institute of Aeronautics and Astronautics (AIAA)

    Kuang-Ying Ting

  2. Aeroservoelastic Wind Tunnel Evaluation of H∞ Active Flutter Suppression

    Article • January 2026, American Institute of Aeronautics and Astronautics (AIAA)

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  3. Destabilize/Stabilize Approach to Experimental Active Flutter Suppression Technology Development

    Article • Journal of Guidance Control and Dynamics, May 2025, American Institute of Aeronautics and Astronautics (AIAA)

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  4. A Destabilize/Stabilize Approach to Experimental Active Flutter Suppression Technology Development

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

    Kuang-Ying Ting

  5. Test/Analysis Active Control Exploration Using the University of Washington’s Multiple Control Surface Large FlexibleWing

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

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  6. Supersonic Configurations at Low Speeds (SCALOS): Wind Tunnel Tests at the University of Washington - an Overview and Some Key Insights

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

    Kuang-Ying Ting

  7. Supersonic Configurations at Low Speeds (SCALOS) Lateral-Directional Aerodynamics: Configuration Variations and Control Surface Effects

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

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  8. Supersonic Configurations at Low Speeds(SCALOS): Correlation of CFD and Wind Tunnel Test Results

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

    Kuang-Ying Ting

  9. Supersonic Configurations at Low Speeds (SCALOS): Wind Tunnel Correction

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

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  10. Supersonic Configurations at Low Speeds (SCALOS): Wind Tunnel Progress

    Article • January 2024, American Institute of Aeronautics and Astronautics (AIAA)

    Kuang-Ying Ting

  11. Aeroservoelastic Wind Tunnel Evaluation of Preview H2 and H∞ Gust Load Alleviation

    Article • Journal of Guidance Control and Dynamics, November 2023, American Institute of Aeronautics and Astronautics (AIAA)

    Kuang-Ying Ting