Hypersonic Cruise Vehicle Wing Structure Evaluation
NASA Innovation Fund 2010 Project Elastically Shaped Future Air Vehicle Concept
A Contribution to the Theory of Multiweb Wing Structures
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
A Design Summary of Stall Characteristics of Straight Wing Aircraft
The NASA Supercritical-Wing Technology
Kasprzyk Airfoil. The First Wind-Tunnel Tests
Aerodynamics of the Model Airplane. Part 1 - Airfoil Measurements
Design and Experimental Results for the S414 Airfoil