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title: Aircraft Aerodynamic Design
Longitudinal aerodynamic characteristics of light, twin-engine, propeller-driven airplanes
Blade and Trajectory Optimization of a Propeller-Driven Electric Aircraft with Acoustic Constraints
Two-Stage Axial Compressor Rig Designed To Develop and Validate Advanced Aerodynamic Technologies
Aerodynamic characteristics of a large-scale, twin tilt-nacelle V/STOL model
Advanced supersonic cruise aircraft technology
Aerodynamic surface distension system for high angle of attack forebody vortex control
Flutter testing of modern aircraft
Fundamental aerodynamic characteristics of delta wings with leading-edge vortex flows
The NASA Aircraft Energy Efficiency program
Free wing assembly for an aircraft
Aero-Propulsive Modeling for eVTOL Aircraft Using Wind Tunnel Testing with Multisine Inputs
Aerodynamic Characteristics of a Number of Modified NACA Four-Digit-Series Airfoil Sections
Lateral-directional aerodynamic characteristics of light, twin-engine, propeller driven airplanes
Computational and experimental studies of light twin aerodynamic interference
Current Methods Modeling and Simulating Icing Effects on Aircraft Performance, Stability, Control