| A Novel Experiment to Understand the Dynamic Stall Phenomenon in Rotor Axial Flight |
8 |
| Wind Tunnel Test of the SMART Active Flap Rotor |
5 |
| Analysis of Dynamic Stall Mechanisms in Helicopter Rotor Environment |
5 |
| Effect of Sweep on a Pitching Finite Wing |
4 |
| Using Control Redundancy for Power and Vibration Reduction on a Compound Helicopter at High Speeds |
4 |
| The Tip Vortex System of a Four-Bladed Rotor in Dynamic Stall Conditions |
4 |
| A Method for Approximate Prediction of Laminar-Turbulent Transition on Helicopter Rotors |
3 |
| Using Control Redundancy for Power and Vibration Reduction on a Coaxial Rotor Helicopter at High Speeds |
3 |
| Wake Characterization of a Free-Flying Model Helicopter in Ground Effect |
3 |
| Numerical Investigations of Dynamic Stall on a Rotor with Cyclic Pitch Control |
3 |
| High-Fidelity Multidisciplinary Design Optimization Methodology with Application to Rotor Blades |
2 |
| Three-Dimensional Solutions for Rotor Blades Using High-Order Geometrical Nonlinear Beam Finite Elements |
2 |
| Aeroelastic Simulation of the Tail Shake Phenomenon |
2 |
| A Computational Fluid Dynamics-Based Viscous Vortex Particle Method for Coaxial Rotor Interaction Calculations in Hover |
2 |
| Blade Tip Pressure Measurements Using Pressure-Sensitive Paint |
2 |
| A Python-Based Framework for Computationally Efficient Trim and Real-Time Simulation Using Comprehensive Analysis |
2 |
| Characterizing Cycle-to-Cycle Variations in Dynamic Stall Measurements |
2 |
| A Dynamic-Inflow-Based Induced Power Model for General and Optimal Rotor Performance |
2 |
| Generalized Aerodynamic Optimization of Hovering Coaxial Rotor Blades |
1 |
| Performance and Loads of a Lift Offset Rotor: Hover and Wind Tunnel Testing |
1 |
| Helicopter Fuselage Model Drag Reduction by Active Flow Control Systems |
1 |
| Comparison of Comprehensive Analyses Predicting Whirl Flutter Stability of the Wing and Rotor Aeroelastic Test System |
1 |
| Thermal Expansion of Polyether Ether Ketone Bearing Components |
1 |
| An Evaluation of the Effects of Resolved Shear-Driven Atmospheric Turbulence on Ship Airwakes |
1 |
| Coupled and Multimode Tailboom Vibration Control Using Fluidic Flexible Matrix Composite Tubes |
1 |
| Validation of Higher-Order Interactional Aerodynamics Simulations on Full Helicopter Configurations |
1 |
| Geometrically Nonlinear Free Vibration Analysis of Composite Rotor Blades with Advanced Tip Shapes |
1 |
| Comparison of CAMRAD II and RCAS Predictions of Tiltrotor Aeroelastic Stability |
1 |
| Comparison of Advanced RANS Modeling with Dual-Plane PIV Measurements for a Hovering Rotor |
1 |
| Advances in Rotorcraft Crashworthiness: Trends Leading to Improved Survivability 37th Alexander A-Nikolsky Honorary Lecture |
1 |
| Frequency Domain System Identification of a Robinson R44 in Hover |
1 |
| Flow Field and Efficiency of a Two-Dimensional Inertial Particle Separator |
1 |
| Flight Simulation and Control of a Helicopter Undergoing Rotor Span Morphing |
1 |
| Analysis Methods for Improving Confidence in Material Qualification for Laminated Composites |
1 |
| Rotorcraft Precision Hover Control in Atmospheric Turbulence via Eigenstructure Assignment |
1 |
| Design and Development of a 30 g Cyclocopter |
1 |
| Influence of Scavenge Leg Geometry on Inertial Particle Separator Performance |
1 |
| Coupled and Trimmed Aerodynamic and Aeroacoustic Simulations for Airbus Helicopters' Compound Helicopter RACER |
1 |
| The Effect of Steady and Pulsed Air Jet Vortex Generator Blowing on an Airfoil Section Model Undergoing Sinusoidal Pitching |
1 |
| A Parameter Identification Method for Helicopter Noise Source Identification and Physics-Based Semiempirical Modeling |
1 |
| Passive Flow Control of Dynamic Stall via Surface-Based Trapped Vortex Generators |
1 |
| Performance and Loads Study of a High-Speed Compound Helicopter |
1 |
| Investigation of the Rotor-Obstacle Aerodynamic Interaction in Hovering Flight |
1 |
| Rotor Blade Shed Ice Projectile Length Prediction |
1 |
| In Search of a Rotorcraft Airframe Fatigue Assessment Methodology: Cracking Prediction under Service Loading |
0 |
| Parametric Study of Dynamic Inflow for Single and Coaxial Rotor Systems |
0 |
| Wear Out Model Application to Compute Rotorcraft Component Fatigue Life |
0 |
| Full-Scale Flight-Test Results for a Rotorcraft Safe Landing Area Determination Algorithm for Autonomous and Piloted Landing Approaches |
0 |
| Numerical Assessment of a High Disk Loading Annular Lift Fan Aircraft |
0 |
| Numerical Study of Retreating Side Blowing Concept for a Rotor in High-Speed Flight |
0 |
