Methodology to Create a Unified Trade-Off Environment for Advanced Aerospace Vehicle
Flexible Wing Designs with Sensor Control Feedback for Demonstration on the X-56A (MUTT)
NASA Innovation Fund 2010 Project Elastically Shaped Future Air Vehicle Concept
Design and Experimental Results for the S414 Airfoil
Design and Experimental Results for the S407 Airfoil
Real-time In-Flight Strain and Deflection Monitoring with Fiber Optic Sensors
Energy Based Aerodynamic Modeling: Increasing Fidelity of Fixed-Wing Constructive Entities
Experimental Analysis of Propeller Interactions With a Flexible Wing Micro-Air-Vehicle
Investigation of Transonic Reynolds Number Scaling on a Twin-Engine Transport
Airfoil Dynamic Stall and Rotorcraft Maneuverability
Effects of Large-Droplet Ice Accretion on Airfoil and Wing Aerodynamics and Control
Anti-Symmetric Mode Flutter of Winged Reentry Space Vehicle
Large Capacity Oblique All-Wing Transport Aircraft
Design Methodology for Multi-Element High-Lift Systems on Subsonic Civil Transport Aircraft