Mars Helicopter Technology Demonstrator
The Digital Twin Paradigm for Future NASA and U.S. Air Force Vehicles
Application of Convolutional Neural Network to Predict Airfoil Lift Coefficient
Application of Focused Laser Differential Interferometry (FLDI) in a Supersonic Boundary Layer
Experimental Study of Quadcopter Acoustics and Performance at Static Thrust Conditions
An Experimental Investigation on Rotor-to-Rotor Interactions of Small UAV Propellers
Experimental Study of a CFD Validation Test Case for Turbulent Separated Flows
Description and assessment of the new ONERA 2D icing suite IGLOO2D
An Efficient Parallel Overset Method for Aerodynamic Shape Optimization
Initial Investigation into the Psychoacoustic Properties of Small Unmanned Aerial System Noise
A Vehicle Design and Optimization Model for On-Demand Aviation
Extending the Gamma-Rethetat Correlation based Transition Model for Crossflow Effects (Invited)
Experimental Investigation of Airfoil Turbulence-Impingement Noise Reduction Using Porous Treatment
Detonation Wave Dynamics in a Rotating Detonation Engine
Hypersonic Ground Tests In Support of the Boundary Layer Transition (BOLT) Flight Experiment