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- > Flight Investigation of Coaxial Rotor Tip Vortex Structure
- > Rotor-Fuselage Vibration Analysis for A Dissimilar Rotor with Single and Multiple Faults
- > Control Design And Assessment Of Active Trailing Edge Actuators For A Model Rotor
- > Oscillating Iced Airfoil Pressure Measurement and Computation
- > 39th Annual Vertical Flight Society Student Design Competition - OLIWHOPER
- > Computational Simulation and Analysis of Bell/Boeing Quad Tiltrotor Aero Interaction Using a Navier-Stoke Flow Solver
- > Minimum-Induced Power Loss of a Helicopter Rotor via Circulation Optimization
- > The Aviation Turbine Engine Diagnostics System (ATEDS), An Effective Tool For Army Maintenance
- > Experimental/Numerical Evaluation Of Integral Trailing Edge Flaps For Helicopter Rotor Applications
- > Prediction and Validation of Sloshing and Fluid-Structure Interactions Using FPM for VTOL Applications
- > Belt Mounted Airbag System for Use in Helicopter Applications
- > Performance Evaluation of Full Scale On-board Active Flap System in Transonic Wind Tunnel
- > Development of an Improved Deice System for UH-60 Rotor Blades
- > Comprehensive Analysis, Prediction, and Validation of UH-60A Blade Loads in Unsteady Maneuvering Flight
- > Improved Prediction of Rotor Maneuvering Loads using Hybrid Methodology
- > Preliminary Study Of The Turboshaft Selection For A Helicopter Upgrade Program
- > Towards CFD Simulations of Transient Tiltrotor Conversion Maneuvers
- > Sense and Respond Logistics: Supporting Warfighter Replenishment with Mule UAV
- > Future Directions for an Industry in a Challenging Budget Environment - Lockheed Martin
- > Method for Predicting Multi-Axis Task Performance and Handling Qualities Rating for a Coaxial-Compound and Tiltrotor Rotorcraft with Validating Data
- > VTOL Hybrid Airship Review
- > Enhanced Aviator Protection In Survivable Crashes Using A Restraint Pretensioner
- > Component Fatigue Life Reliability with Usage Monitor
- > Gearbox Casing Crack Detection based on Vibration Signals in Frequency and Time Domain
- > Development of Modern Control Laws for the AH-64D in Hover/Low Speed Flight
- > Results of a Viscous Flow Analysis for Proprotor Design
- > The Next Generation of Army Aviation Systems
- > Bell's Model 427 - An Affordable Light Twin Helicopter
- > Flight Demonstration of an Adaptive Guidance Controller for Autonomous Formation Flight
- > A Comparative Analysis of Three Composite Fuselage Concepts for Crash Performance
- > Development of an Operational Analysis Tool for Urban Air Mobility
- > Coaxial Rotor Performance and Wake Dynamics in Steady and Manoeuvring Flight
- > Control Law Design for Compliance with ADS-33C Failure State Requirements, the Comanche Approach
- > Evaluation of Limited Authority Attitude Command Architectures for Rotorcraft
- > Numerical Investigation of Rotorcraft Fuselage Drag Reduction using Active Flow Control
- > Optimal OEI Clear Heliport Operation of a Multiengine Helicopter
- > Predicting the Onset of the Vortex Ring State Under Accelerated Flight Conditions
- > NASA - New Direction for Vertical Lift Research
- > Online Detection and Avoidance of Helicopter TGT Limits
- > V-22 Osprey Qualification Testing Leading to Flight in Known Icing Conditions
- > Straight Talk with the CEO - Sikorsky
- > An Enhanced HUMS Foundation for Rotorcraft IVHM
- > Comparative Study Of Vibration Condition Indicators For Crack Detection In Spur Gears
- > Concept Level Topology Optimization of an AAM Fuselage
- > Innovative Systems to Reduce One Per Rev Vibrations in Helicopters
- > Design and Initial Flight Testing of a Coaxial Tilting-Head Compound Rotorcraft
- > Overview of the Testing of a Small-Scale Proprotor
- > NASA Revolutionary Vertical Lift Technology (RVLT)
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