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1. The Aeromechanical Stability of Soft-Inplane Tiltrotors

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2. DESIGN OF A CENTRIFUGE AND AERODYNAMIC TESTING APPARATUS FOR EVALUATING THE PERFORMANCE OF A NOVEL TRAILING-EDGE FLAP ACTUATOR

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5. ROTOR HUB VIBRATION AND BLADE LOADS REDUCTION, AND ENERGY HARVESTING VIA EMBEDDED RADIAL OSCILLATOR

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6. Shipboard Helicopter Gust Response Alleviation Using Active Trailing Edge Flaps

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8. CHARACTERIZATION AND MODELING OF A FLEXIBLE MATRIX COMPOSITE MATERIAL FOR ADVANCED ROTORCRAFT DRIVELINES

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10. Flight Control Design for Rotorcraft with Variable Rotor Speed

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12. Quasi-static rotor morphing concepts for rotorcraft performance improvements

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14. Nonlinear Active Vibration Based Damage Detection and Localization

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17. Vibration energy harvesting from rotorcraft drive systems using thermoelectric conversion of heat generated by mechanical damping

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19. Comprehensive Model and Experimental Validation of Passive Vibration Suppression for Supercritical Rotary Machines

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20. Rotorcraft Simulations with Coupled Flight Dynamics, Free Wake, and Acoustics

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21. A UNIFIED FLIGHT CONTROL METHODOLOGY FOR A COMPOUND ROTORCRAFT IN FUNDAMENTAL AND AEROBATIC MANEUVERING FLIGHT

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24. MODELING FOR POLYMER/ CARBON NANOTUBE NANOCOMPOSITE TO ESTIMATE STRUCTURAL DAMPING IN A ROTOCRAFT BLADE

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25. Fluidic Flexible Matrix Composite Vibration Treatments for Helicopter Airframes and Rotor Blades

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26. Rotorcraft Flight Control Design with Alleviation of Unsteady Rotor Loads

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27. Fluidic Flexible Matrix Composite Damped Vibration Absorbers for Stiff-Inplane Hingeless Rotor Blades

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28. Design, Development, and Field Testing of the GlacierHawk: an Unmanned Aerial System for Geoscience Data Retrieval

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29. Time-Domain Aeroelastic Stability Predictions of a Semi-Span Tiltrotor

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30. Passive Balancer Development for Rotor Systems in Icing Conditions

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31. Fiber Reinforced Composites with Carbon Nanotubes for Structural Damping of a Rotorcraft Blade

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32. Design, Development, and Tuning of a Gimbaled Coaxial UAV

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33. Benefits of Parallel Hybrid Electric Propulsion for Aircraft and Rotorcraft

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34. Structural Design of a Rigid Coaxial Rotor System for Wind Tunnel Testing

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35. Helicopter Noise Modeling With Varying Fidelity Prediction Systems

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36. Individual Blade Pitch Control (IBC) for Vibration Reduction of Lift-offset Coaxial Rotor Vehicles with Auxiliary Propulsion

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