All Stories

  1. Dynamic Condensation for Efficient Band-Structure Calculations of 2D Periodic Structures

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

    Prof. Jae-Hung Han

  2. Leading-Edge Curvature Effect on Flapping Performance of Low Aspect Ratio Wings in Forward Flight

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

    Prof. Jae-Hung Han, Dr. Reynolds Addo-Akoto

  3. Simplifying Complex Structures: A Faster Way to Predict Vibrations

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

    Prof. Jae-Hung Han, Robel Hagos

  4. Modified Iterative-Order-Reduction Substructuring Method with Interface Boundary Reduction

    Article • AIAA Journal, October 2023, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jae-Hung Han

  5. Rigid-Foldable Polyhedral Origami

    Article • AIAA Journal, October 2023, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jae-Hung Han

  6. Multiple-Input/Multiple-Output Random Vibration Control for Simulating a Horizontal Direction Launch Environment

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

    Prof. Jae-Hung Han

  7. Publisher's Note: “Aerodynamic characteristics of flexible flapping wings depending on aspect ratio and slack angle” [Phys. Fluids 34, 051911 (2022)]

    Article • Physics of Fluids, June 2022, American Institute of Physics

    Prof. Jae-Hung Han, Dr. Reynolds Addo-Akoto

  8. Aerodynamic characteristics of flexible flapping wings depending on aspect ratio and slack angle

    Article • Physics of Fluids, May 2022, American Institute of Physics

    Prof. Jae-Hung Han, Dr. Reynolds Addo-Akoto

  9. Self-Learning MAV Under Safety-Guaranteed Flight Test Environment

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

    Prof. Jae-Hung Han

  10. Automated Aerial Docking System Using Onboard Vision-Based Deep Learning

    Article • Journal of Aerospace Information Systems, March 2022, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jae-Hung Han

  11. Aeroelastic Behavior of Two Airfoils in Proximity

    Article • AIAA Journal, October 2021, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jae-Hung Han

  12. New Approach to Folding a Thin-Walled Yoshimura Patterned Cylinder

    Article • Journal of Spacecraft and Rockets, December 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jae-Hung Han

  13. Performance Optimization of a Split-Type Low-Shock Separation Bolt

    Article • Journal of Spacecraft and Rockets, September 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jae-Hung Han, Dae-Hyun Hwang

  14. Ground Effect on Flutter and Limit Cycle Oscillation of Airfoil with Flap

    Article • Journal of Aircraft, August 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jae-Hung Han

  15. Separation Behavior of Pyrotechnically Actuated Device Considering Small-Volume Effect of Combustion Chamber

    Article • Journal of Spacecraft and Rockets, July 2020, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jae-Hung Han, Dae-Hyun Hwang, Junsu Shin

  16. Interactions of the wakes of two flapping wings in hover

    Article • Physics of Fluids, February 2019, American Institute of Physics

    Prof. Jae-Hung Han, Jong-Seob Han

  17. Performance optimization of a split type low-shock separation bolt

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

    Prof. Jae-Hung Han, Dae-Hyun Hwang

  18. Development of Pyroshock Simulator for Shock Propagation Test

    Article • Shock and Vibration, September 2018, Hindawi Publishing Corporation

    Dae-Hyun Hwang, Prof. Jae-Hung Han

  19. Mathematical Model for the Separation Behavior of Low-Shock Separation Bolts

    Article • Journal of Spacecraft and Rockets, September 2018, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jae-Hung Han, Dae-Hyun Hwang

  20. The Trim Condition of a Hovering Insect-like Flapping-wing Micro Air Vehicle in Asymmetric Condition

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

    Prof. Jae-Hung Han

  21. An efficient aerodynamic model for flapping insects

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

    Prof. Jae-Hung Han, Jong-Seob Han

  22. Safety-Guaranteed Flight Test Environment for Micro Air Vehicles

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

    Prof. Jae-Hung Han

  23. Dynamic Stability of a Hawkmoth-scale Flapping-wing Micro Air Vehicle during Forward Flight

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

    Prof. Jae-Hung Han, Jong-Seob Han

  24. Effects of Advance Ratio on the Aerodynamic Characteristics of an Insect Wing in Forward Flight

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

    Prof. Jae-Hung Han, Jong-Seob Han

  25. Design of Three Parameter Isolator for the RWA Disturbance Considering Flexible Structural Effects

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

    Prof. Jae-Hung Han

  26. An improved quasi-steady aerodynamic model for insect wings that considers movement of the center of pressure

    Article • Bioinspiration & Biomimetics, July 2015, Institute of Physics Publishing

    Prof. Jae-Hung Han

  27. Role of Trailing-Edge Vortices on the Hawkmothlike Flapping Wing

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

    Prof. Jae-Hung Han, Jong-Seob Han

  28. Design of frequency-tunable mesh washer isolators using shape memory alloy actuators

    Article • Journal of Intelligent Material Systems and Structures, June 2015, SAGE Publications

    Prof. Jae-Hung Han

  29. Longitudinal Stabilization of Hovering Flapping Wing Air Vehicles

    Article • Journal of Guidance Control and Dynamics, April 2015, American Institute of Aeronautics and Astronautics (AIAA)

    Prof. Jae-Hung Han

  30. Parametric investigation on plasma streamwise vortex generators with flow around the bluff body

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

    Prof. Jae-Hung Han

  31. Safety-guaranteed Flight Test Environment for Micro Air Vehicles

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

    Prof. Jae-Hung Han

  32. One-equation modeling and validation of dielectric barrier discharge plasma actuator thrust

    Article • Journal of Physics D Applied Physics, September 2014, Institute of Physics Publishing

    Prof. Jae-Hung Han

  33. Development of multi-degree-of-freedom microvibration emulator for efficient jitter test of spacecraft

    Article • Journal of Intelligent Material Systems and Structures, February 2014, SAGE Publications

    Prof. Jae-Hung Han

  34. Experimental Study on the Unsteady Aerodynamics of a Robotic Hawkmoth Manduca sexta model

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

    Prof. Jae-Hung Han

  35. Control of Wing Stroke Plane Angle for Stabilizing of a Hovering Flapping-Wing Air Vehicle

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

    Prof. Jae-Hung Han