| Issues in Deciding Whether to Use Multifidelity Surrogates |
16 |
| Aircraft Icing Severity Analysis Considering Three Uncertainty Types |
14 |
| Nonlinear Model Order Reduction via Lifting Transformations and Proper Orthogonal Decomposition |
14 |
| Active and Passive Turbulent Boundary-Layer Drag Reduction |
13 |
| Analysis of Dynamic Stall on a Pitching Airfoil Using High-Fidelity Large-Eddy Simulations |
13 |
| Fundamental Properties of Fluidic Oscillators for Flow Control Applications |
12 |
| Multirotor Drone Noise at Static Thrust |
12 |
| Hierarchical Nondeterministic Optimization of Curvilinearly Stiffened Panel with Multicutouts |
11 |
| Aerodynamic Shape Optimization of Natural-Laminar-Flow Wing Using Surrogate-Based Approach |
11 |
| Flow Separation Control over a NACA 0015 Airfoil Using Nanosecond-Pulsed Plasma Actuator |
11 |
| Aerodynamic Design of the Hyperloop Concept |
10 |
| Flow Control of Tip/Edge Vortices |
10 |
| Flowfield Reconstruction Method Using Artificial Neural Network |
10 |
| Unsteady Flow Physics of Airfoil Dynamic Stall |
9 |
| Phase-Synchronized Fluidic Oscillator Pair |
9 |
| Flow Physics and Frequency Scaling of Sweeping Jet Fluidic Oscillators |
9 |
| Multifidelity Uncertainty Propagation via Adaptive Surrogates in Coupled Multidisciplinary Systems |
9 |
| Reynolds Number Scaling of the Propulsive Performance of a Pitching Airfoil |
9 |
| Numerical Study on Thermodynamic Efficiency and Stability of Oblique Detonation Waves |
9 |
| Benchmark Aerostructural Models for the Study of Transonic Aircraft Wings |
9 |
| Overview of Turbulent Inflow Boundary Conditions for Large-Eddy Simulations |
8 |
| Proper-Orthogonal-Decomposition-Based Buckling Analysis and Optimization of Hybrid Fiber Composite Shells |
8 |
| Wall-Modeled Large-Eddy Simulation of Transonic Airfoil Buffet at High Reynolds Number |
8 |
| Computational Fluid Dynamic Analysis of Fluidic Actuator for Active Flow Control Applications |
8 |
| Flow-Separation Control Using Sweeping Jet Actuator |
8 |
| Exploration of High-Frequency Control of Dynamic Stall Using Large-Eddy Simulations |
8 |
| Inverse Design of Airfoil Using a Deep Convolutional Neural Network |
8 |
| Greedy Nonintrusive Reduced Order Model for Fluid Dynamics |
8 |
| Multifidelity Surrogate Based on Single Linear Regression |
8 |
| Prestressed Vibration of Stiffened Variable-Angle Tow Laminated Plates |
7 |
| Direct Numerical Simulation of Transcritical Jets at Moderate Reynolds Number |
7 |
| Transition Between Different Initiation Structures of Wedge-Induced Oblique Detonations |
7 |
| Unsteady Lift and Moment of a Periodically Plunging Airfoil |
7 |
| Unsteady Vortex Structure Induced by a Trielectrode Sliding Discharge Plasma Actuator |
7 |
| Enhanced Supersonic Combustion Targeting Combustor Length Reduction in a Mach 12 Scramjet |
7 |
| Vibration Tests of 3D Printed Satellite Structure Made of Lattice Sandwich Panels |
7 |
| Component-Based Geometry Manipulation for Aerodynamic Shape Optimization with Overset Meshes |
7 |
| Wind-Turbine Trailing-Edge Noise Reduction by Means of Boundary-Layer Suction |
7 |
| Direct Numerical Simulation Database for Supersonic and Hypersonic Turbulent Boundary Layers |
7 |
| Endothermic Pyrolysis of JP-10 with and without Zeolite Catalyst for Hypersonic Applications |
7 |
| Vibration of Laminated Composite Shells with Cutouts and Concentrated Mass |
7 |
| Engineering Design with Digital Thread |
7 |
| Control of Dynamic Stall over a NACA 0015 Airfoil Using Plasma Actuators |
7 |
| Flight Test of an Active Flow Control Enhanced Vertical Tail |
7 |
| Numerical Study on Liquid Droplet Internal Flow Under Shock Impact |
7 |
| Investigating the Aeroelastic Behaviors of Rotor Blades with Nonlinear Energy Sinks |
7 |
| Turbofan Broadband Noise Prediction Using the Lattice Boltzmann Method |
7 |
| Turbulence Intensity Effects on Laminar Separation Bubbles Formed over an Airfoil |
7 |
| Heat Transfer in Nonequilibrium Flows with Homogeneous and Heterogeneous Recombination Reactions |
6 |
| Method of Investigation for Numerical Simulation on Aero-Optical Effect Based on WCNS-E-5 |
6 |
