APPLICATION OF BOUNDARY LAYER INGESTION TO AN UNMANNED AIR VEHICLE
Flight Test of Stable Automated Cruise Flap for an Adaptive Wing Aircraft
Development of Stable Automated Cruise Flap for an Aircraft with Adaptive Wing
Design of Launch Vehicle Flight Control Systems Using Ascent Vehicle Stability Analysis Tool
Mechanical Slosh Models for Rocket-Propelled Spacecraft (AIAA 2013-4651)