NASA Innovation Fund 2010 Project Elastically Shaped Future Air Vehicle Concept
Aerodynamic Characteristics of a Swept Augmentor Wing
Flexible Wing Designs with Sensor Control Feedback for Demonstration on the X-56A (MUTT)
Hypersonic Aerodynamic Characteristics of a Flat-Top Wing Body Combination
Aerodynamics of the Model Airplane. Part 1 - Airfoil Measurements
Design and Experimental Results for the S414 Airfoil
Aerodynamic Optimization of Wings at Subsonic Speeds and the Influence of Wingtip Design
Large Capacity Oblique All-Wing Transport Aircraft
Aerodynamic Characteristics of Slender Wings in Ground Proximity
Transonic Flutter Study of a Wind-Tunnel Model of a Supercritical Wing with/Without Winglet
Effect of Flap Deflection on the Lift Coefficient of Wings Operating in a Biplane Configuration
Experimental Study of Flow About a Stalled Two-Dimensional Airfoil