Coupled Boundary-Layer Suction and Airfoil Optimization for Hybrid Laminar Flow Control
Numerical Simulation of Iced Wing Using Separating Shear Layer Fixed Turbulence Models
Experimental and Numerical Analysis of a Streamwise Vortex Downstream of a Delta Wing
Automated Mesh Deformation for Computer-Aided Design Models That Exhibit Boundary Topology Changes
Overview of Unsteady Aerodynamic Response of Rigid Wings in Gust Encounters
Effect of Sweep on Dynamic Stall of a Pitching Finite-Aspect-Ratio Wing
Multiple Thermal Updraft Estimation and Observability Analysis
Mitigation of Dynamic Stall over a Pitching Finite Wing Using High-Frequency Actuation
Log Polynomial Velocity Profile for Vertical Landing
Dynamic Stall of a Finite-Aspect-Ratio Wing
Extension of a Reynolds-Stress-Based Transition Transport Model for Crossflow Transition
Lift Prediction Including Stall, Using Vortex Lattice Method with Kirchhoff-Based Correction
Stall Recovery of a Morphing Wing via Extended Nonlinear Lifting-Line Theory
Two-Step Stall Characteristic of an Airfoil with a Single Leading-Edge Protuberance
Extension of a Two-Dimensional Navier–Stokes Solver for Infinite Swept Flow
Downwash Detection and Avoidance with Small Quadrotor Helicopters
Exit-Slot Orientation on Pumping Blades for a Rotor in Ground Effect
Numerical Study on Transitional Flows Using a Correlation-Based Transition Model
Modifying Low-Drag Bodies to Generate Lift: A Computational Study
Numerical Study of the Reliability of Wind-Tunnel Wall Corrections for Wingtip Flow
Model for Longitudinal Perch Maneuvers of a Fixed-Wing Unmanned Aerial Vehicle
Development of a Quasi-Static Span-Extending Blade Tip for a Morphing Helicopter Rotor
Role of Trailing-Edge Vortices on the Hawkmothlike Flapping Wing
Enhancement of a Correlation-Based Transition Turbulence Model for Simulating Crossflow Instability
Uncertainty Quantification for Airfoil Icing Using Polynomial Chaos Expansions
Effect of Root Cutout on Force Coefficients of Rotating Wings
Low-Order Modeling of the Unsteady Aerodynamics in Flapping Wings
Swept-Wing Boundary-Layer Transition and Turbulent Flow Physics from Multipoint Measurements
Aerodynamic Design Optimization Studies of a Blended-Wing-Body Aircraft
Extended Formation Flight at Transonic Speeds
Experimental and Analytic Investigation of Ground Effect
Leading-Edge Vortex Structure over Multiple Revolutions of a Rotating Wing
Biplane and Tail Effects in Flapping Flight
Methodology to Create a Unified Trade-Off Environment for Advanced Aerospace Vehicle
Flexible Wing Designs with Sensor Control Feedback for Demonstration on the X-56A (MUTT)
Time-Optimal Path Following for Fixed-Wing Aircraft
NASA Innovation Fund 2010 Project Elastically Shaped Future Air Vehicle Concept
Design and Experimental Results for the S414 Airfoil
Boundary-Layer Transition on Broad Cones rotating in an Imposed Axial Flow
Design and Experimental Results for the S407 Airfoil
Implicit Large-Eddy Simulation of Swept-Wing Flow Using High-Resolution Methods
Geometry Parameterization Method for Multidisciplinary Applications
Improvement of Delayed-Detached Eddy Simulation Applied to Separated Flow over Missile Fin