AIAA-2004-5071 Towards Desgn of Long-Range Supersonic Military Aircraft
AIAA-2004-5070 Towards Design of Mach 1.6+ Supersonic Cruise Aircraft
AIAA-2003-6725 Airborne Conflict Resolution for Flow-Restricted Transition Airspace
Leading Edge Vortex Flaps on Moderate Sweep Wings- UCAV, Flow Improvement at High Lift AIAA Paper
Morphing UCAV Wings Incorporating In-plane & Folding Tips - aerodynamic Design Studies