Active Circulation Control on the Blunt Trailing Edge Wind Turbine Airfoil
Additive Manufacturing of Solid Rocket Propellant Grains
Adjoint-Based Optimization of Three-Dimensional Flapping-Wing Flows
Adjoint-Based Sensitivity Formulation for Fully Coupled Unsteady Aeroelasticity Problems
Adjoint-Based Shape Optimization for Electromagnetic Problems Using Discontinuous Galerkin Methods
Advanced Kinematic Tailoring for Morphing Aircraft Actuation
Aerodynamic Load Control for Multi-Element Airfoils Using Surface-Normal Trailing-Edge Blowing
Aerodynamic Loads and Moments on Axisymmetric Ring-Wing Ducts
Aerodynamic Performance and Wake Development of Airfoils with Serrated Trailing-Edges
Aerodynamic Shape Optimization of Aircraft Wings Using Panel Methods
Aerodynamic Shape Optimization of Highly Nonplanar Raised and Drooped Wings
Aerodynamic Shape Optimization of Wings Using a Parallel Newton-Krylov Approach
Aerodynamic Shape Optimization Using Geometry Surrogates and Adjoint Method
Aerodynamics of a Common Research Model Wing with Leading-Edge Ice Shape
Aeroelastic Design of Blended Composite Structures Using Lamination Parameters
Aeroelastic Optimization of Aircraft Wings Using a Coupled Three-Dimensional Panel-Beam Model
Aeroelastic Rotorcraft–Pilot Couplings in Tiltrotor Aircraft
Airfoil Data Fitting Using Multivariate Smoothing Thin Plate Splines
Approach to Aerodynamic Design Through Numerical Optimization
Assessing the Usability of Two Declarative Programming Languages to Model Geometric Events
Automated Mesh Generation and Solution Analysis of Arbitrary Airfoil Geometries
Automatic Design of Wing–Body–Nacelle Configurations for Minimum Drag
Basic Understanding of Airfoil Characteristics at Low Reynolds Numbers ()
Benchmark Aerostructural Models for the Study of Transonic Aircraft Wings
Broadband Shock-Associated Noise in Screeching and Non-Screeching Underexpanded Supersonic Jets
Cavities Improve the Power Factor of Low-Reynolds-Number Airfoils and Wings
Compact, Efficient Wing Geometries for Micro Aerial Vehicles
Comparison of Theoretical and Multifidelity Optimum Aerostructural Solutions for Wing Design
Component-Mode Reduced-Order Models for Geometric Mistuning of Integrally Bladed Rotors
Computational Analysis of Vortex Wakes Without Near-Field Rollup Characteristics
Computational and Experimental Validation of the Active Morphing Wing
Control of Poststall Airfoil Using Leading-Edge Pulsed Jets
Convergence Error and Higher-Order Sensitivity Estimations
Correction: Optimal Hyperelliptic Cambered Span Configurations for Minimum Drag
Coupling Modes of an Underexpanded Twin Axisymmetric Jet
Criteria for Vortex Breakdown Above High-Sweep Delta Wings
Critical Protuberance Height for Transition of Leading Edge Boundary Layers
Cross Validation of Aerodynamic Shape Optimization Methodologies for Aircraft Wing-Body Optimization
Data-Based Approach for Fast Airfoil Analysis and Optimization