| Basic Understanding of Airfoil Characteristics at Low Reynolds Numbers (10(4)-10(5)) |
16 |
| Aircraft Active Flutter Suppression: State of the Art and Technology Maturation Needs |
10 |
| Aerodynamic Modeling, System Identification, and Analysis of Iced Aircraft Configurations |
9 |
| Design of a New Magnetorheological Damper Based on Passive Oleo-Pneumatic Landing Gear |
8 |
| Control of Landing Efficiency of an Aircraft Landing Gear System With Magnetorheological Dampers |
7 |
| Minimizing Induced Drag with Lift Distribution and Wingspan |
6 |
| Fuel-Efficient Trajectories Traffic Synchronization |
6 |
| Numerical Study of Iced Airfoils with Horn Features Using Large-Eddy Simulation |
6 |
| Modeling Boundary Layer Ingestion Using a Coupled Aeropropulsive Analysis |
6 |
| Summary Data from the Sixth AIAA CFD Drag Prediction Workshop: CRM Cases |
6 |
| Higher-Order Free-Wake Method for Propeller-Wing Systems |
5 |
| Evaluating Energy-Saving Arrivals of Wide-Body Passenger Aircraft via Flight-Simulator Experiments |
5 |
| High-Fidelity Design-Allocation Optimization of a Commercial Aircraft Maximizing Airline Profit |
5 |
| Application of Vortex Methods to Coaxial Rotor Wake and Load Calculations in Hover |
5 |
| Overview and Summary of the Third AIAA High Lift Prediction Workshop |
5 |
| Preliminary Sizing Method for Hybrid-Electric Distributed-Propulsion Aircraft |
5 |
| Droplet Breakup Criterion in Airfoils Leading Edge Vicinity |
4 |
| Control of Transonic Buffet by Shock Control Bumps on Wing-Body Configuration |
4 |
| Modeling and Adaptive Flight Control for Quadrotor Trajectory Tracking |
4 |
| Performance Improvement of Small Unmanned Aerial Vehicles Through Gust Energy Harvesting |
4 |
| Design, Manufacturing and Wind Tunnel Validation of a Morphing Compliant Wing |
4 |
| Three-Dimensional Ice-Accretion Measurement Methodology for Experimental Aerodynamic Simulation |
4 |
| Aeromechanics Analysis of a High-Advance-Ratio Lift-Offset Coaxial Rotor System |
4 |
| Mission Analysis and Component-Level Sensitivity Study of Hybrid-Electric General-Aviation Propulsion Systems |
4 |
| New Robust Method to Study Flight Flutter Testing |
4 |
| Procedure for Determining Operation Limits of High-Altitude Long-Endurance Aircraft Under Icing Conditions |
4 |
| UH-60A Rotor Performance and Loads Correlation at High Advance Ratios |
4 |
| Retrospective on the Common Research Model for Computational Fluid Dynamics Validation Studies |
4 |
| Nonlinear Aeroelastic Control of Very Flexible Aircraft Using Model Updating |
4 |
| Summary of Propagation Cases of the Second AIAA Sonic Boom Prediction Workshop |
3 |
| Stabilized Finite Elements in FUN3D |
3 |
| Nearfield Summary and Statistical Analysis of the Second AIAA Sonic Boom Prediction Workshop |
3 |
| Underactuated Stratospheric Airship Trajectory Control Using an Adaptive Integral Backstepping Approach |
3 |
| Deformation Control of Highly Flexible Aircraft in Trimmed Flight and Gust Encounter |
3 |
| RANS-Based Aerodynamic Shape Optimization of a Strut-Braced Wing with Overset Meshes |
3 |
| Assessing Calculated Blade Loads of the Tilt Rotor Aeroacoustic Model |
3 |
| Noise Characterization of a Full-Scale Nose Landing Gear |
3 |
| Study on Heating Strategies of Nose Cone Electrothermal Anti-Icing |
3 |
| Vortex Approach for Downwash and Outwash of Tandem Rotors in Ground Effect |
3 |
| Alleviation of Propeller-Slipstream-Induced Unsteady Pylon Loading by a Flow-Permeable Leading Edge |
3 |
| Improving Aircraft Noise Predictions Considering Fan Rotational Speed |
3 |
| Parametric Study of Propeller Whirl Flutter Stability with Full-Span Model of X-57 Maxwell Aircraft |
3 |
| Solar and Gas Powered Long-Endurance Unmanned Aircraft Sizing via Geometric Programming |
3 |
| Numerical Simulations of Low-Reynolds-Number Flow Past Finite Wings with Leading-Edge Protuberances |
3 |
| Transitional Flight of Tail-Sitter Unmanned Aerial Vehicle Based on Multiple-Model Adaptive Control |
3 |
| DPW-6: Drag Analyses and Increments Using Different Geometries of the Common Research Model Airliner |
3 |
| Multidisciplinary Optimization of Unmanned Aircraft Considering Radar Signature, Sensors, and Trajectory Constraints |
3 |
| Designing Wing Twist or Planform Distributions for Specified Lift Distributions |
3 |
| Aerodynamic Load Alleviation Using Minitabs |
3 |
| Observability and Performance Analysis of a Model-Free Synthetic Air Data Estimator |
3 |
